1 /**********************************************************************
3 FILENAME: uiuc_aircraft.h
5 ----------------------------------------------------------------------
7 DESCRIPTION: creates maps for all keywords and variables expected in
8 aircraft input file, includes all parameters that
9 define the aircraft for use in the uiuc aircraft models.
11 ----------------------------------------------------------------------
15 ----------------------------------------------------------------------
19 ----------------------------------------------------------------------
21 HISTORY: 01/26/2000 initial release
22 02/10/2000 (JS) changed aeroData to aeroParts (etc.)
23 added Twin Otter 2.5 equation variables
24 added Dx_cg (etc.) to init & record maps
25 added controlsMixer to top level map
26 02/18/2000 (JS) added variables needed for 1D file
27 reading of CL and CD as functions of alpha
28 02/29/2000 (JS) added variables needed for 2D file
29 reading of CL, CD, and Cm as functions of
30 alpha and delta_e; of CY and Cn as function
31 of alpha and delta_r; and of Cl and Cn as
32 functions of alpha and delta_a
33 03/02/2000 (JS) added record features for 1D and 2D
35 03/29/2000 (JS) added Cmfa interpolation functions
36 and Weight; added misc map
37 04/01/2000 (JS) added throttle, longitudinal, lateral,
38 and rudder inputs to record map
39 03/09/2001 (DPM) added support for gear
40 06/18/2001 (RD) added variables needed for aileron,
41 rudder, and throttle_pct input files.
42 Added Alpha, Beta, U_body, V_body, and
43 W_body to init map. Added variables
44 needed to ignore elevator, aileron, and
45 rudder pilot inputs. Added CZ as a function
46 of alpha, CZfa. Added twinotter to engine
48 07/05/2001 (RD) added pilot_elev_no_check, pilot_ail_no
49 _check, and pilot_rud_no_check variables.
50 This allows pilot to fly aircraft after the
51 input files have been used.
52 08/27/2001 (RD) Added xxx_init_true and xxx_init for
53 P_body, Q_body, R_body, Phi, Theta, Psi,
54 U_body, V_body, and W_body to help in
55 starting the A/C at an initial condition.
56 10/25/2001 (RD) Added new variables needed for the non-
57 linear Twin Otter model at zero flaps
59 11/12/2001 (RD) Added variables needed for Twin Otter
60 non-linear model with flaps (Cxfxxf).
61 Zero flap variables removed.
62 01/11/2002 (AP) Added keywords for bootTime
63 02/13/2002 (RD) Added variables so linear aero model
64 values can be recorded
65 02/18/2002 (RD) Added variables necessary to use the
66 uiuc_3Dinterp_quick() function. Takes
67 advantage of data in a "nice" form (data
68 that are in a rectangular matrix).
69 04/21/2002 (MSS) Added new variables for apparent mass effects
70 and options for computing *_2U coefficient
72 08/29/2002 (MSS) Added simpleSingleModel
73 09/18/2002 (MSS) Added downwash options
74 03/03/2003 (RD) Changed flap_cmd_deg to flap_cmd (rad)
75 03/16/2003 (RD) Added trigger variables
76 08/20/2003 (RD) Removed old_flap_routine. Changed spoiler
77 variables to match flap convention. Changed
78 flap_pos_pct to flap_pos_norm
79 10/31/2003 (RD) Added variables and keywords for pah and alh
81 11/04/2003 (RD) Added variables and keywords for rah and hh
84 ----------------------------------------------------------------------
86 AUTHOR(S): Bipin Sehgal <bsehgal@uiuc.edu>
87 Jeff Scott <jscott@mail.com>
88 Robert Deters <rdeters@uiuc.edu>
89 David Megginson <david@megginson.com>
90 Ann Peedikayil <peedikay@uiuc.edu>
92 ----------------------------------------------------------------------
96 ----------------------------------------------------------------------
100 ----------------------------------------------------------------------
104 ----------------------------------------------------------------------
106 CALLED BY: uiuc_1DdataFileReader.cpp
107 uiuc_2DdataFileReader.cpp
108 uiuc_aerodeflections.cpp
109 uiuc_coefficients.cpp
111 uiuc_initializemaps.cpp
115 ----------------------------------------------------------------------
119 ----------------------------------------------------------------------
121 COPYRIGHT: (C) 2000 by Michael Selig
123 This program is free software; you can redistribute it and/or
124 modify it under the terms of the GNU General Public License
125 as published by the Free Software Foundation.
127 This program is distributed in the hope that it will be useful,
128 but WITHOUT ANY WARRANTY; without even the implied warranty of
129 MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
130 GNU General Public License for more details.
132 You should have received a copy of the GNU General Public License
133 along with this program; if not, write to the Free Software
134 Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301, USA.
136 **********************************************************************/
142 #include <simgear/compiler.h>
144 #include <FDM/LaRCsim/ls_types.h>
150 #include "uiuc_parsefile.h"
151 #include "uiuc_flapdata.h"
153 typedef stack :: iterator LIST;
155 /* Add more keywords here if required*/
156 enum {init_flag = 1000, geometry_flag, controlSurface_flag, controlsMixer_flag,
157 mass_flag, engine_flag, CD_flag, CL_flag, Cm_flag, CY_flag, Cl_flag,
158 Cn_flag, gear_flag, ice_flag, record_flag, misc_flag, fog_flag};
160 // init ======= Initial values for equation of motion
161 // added to uiuc_map_init.cpp
162 enum {Dx_pilot_flag = 2000,
180 recordStartTime_flag,
181 use_V_rel_wind_2U_flag,
182 nondim_rate_V_rel_wind_flag,
183 use_abs_U_body_2U_flag,
185 dyn_on_speed_zero_flag,
186 use_dyn_on_speed_curve1_flag,
187 use_Alpha_dot_on_speed_flag,
188 use_gamma_horiz_on_speed_flag,
189 gamma_horiz_on_speed,
197 ignore_unknown_keywords_flag,
199 use_uiuc_network_flag,
201 outside_control_flag};
203 // geometry === Aircraft-specific geometric quantities
204 // added to uiuc_map_geometry.cpp
205 enum {bw_flag = 3000, cbar_flag, Sw_flag, ih_flag, bh_flag, ch_flag, Sh_flag};
207 // controlSurface = Control surface deflections and properties
208 // added to uiuc_map_controlSurface.cpp
209 enum {de_flag = 4000, da_flag, dr_flag,
210 set_Long_trim_flag, set_Long_trim_deg_flag, zero_Long_trim_flag,
211 elevator_step_flag, elevator_singlet_flag, elevator_doublet_flag,
212 elevator_input_flag, aileron_input_flag, rudder_input_flag, flap_pos_input_flag,
213 pilot_elev_no_flag, pilot_ail_no_flag, pilot_rud_no_flag,
214 flap_max_flag, flap_rate_flag, use_flaps_flag,
215 spoiler_max_flag, spoiler_rate_flag, use_spoilers_flag,
217 aileron_sas_max_flag,
218 aileron_stick_gain_flag,
219 elevator_sas_KQ_flag,
220 elevator_sas_max_flag,
221 elevator_sas_min_flag,
222 elevator_stick_gain_flag,
225 rudder_stick_gain_flag,
226 use_elevator_sas_type1_flag,
227 use_aileron_sas_type1_flag,
228 use_rudder_sas_type1_flag,
229 ap_pah_flag, ap_alh_flag, ap_Theta_ref_flag, ap_alt_ref_flag,
230 ap_rah_flag, ap_Phi_ref_flag, ap_hh_flag, ap_Psi_ref_flag};
232 // controlsMixer == Controls mixer
233 enum {nomix_flag = 5000};
235 //mass ======== Aircraft-specific mass properties
236 // added to uiuc_map_mass.cpp
237 enum {Weight_flag = 6000,
238 Mass_flag, I_xx_flag, I_yy_flag, I_zz_flag, I_xz_flag,
239 Mass_appMass_ratio_flag, I_xx_appMass_ratio_flag,
240 I_yy_appMass_ratio_flag, I_zz_appMass_ratio_flag,
241 Mass_appMass_flag, I_xx_appMass_flag,
242 I_yy_appMass_flag, I_zz_appMass_flag};
244 // engine ===== Propulsion data
245 // added to uiuc_map_engine.cpp
246 enum {simpleSingle_flag = 7000, simpleSingleModel_flag,
247 c172_flag, cherokee_flag, gyroForce_Q_body_flag, gyroForce_R_body_flag,
248 omega_flag, omegaRPM_flag, polarInertia_flag,
249 slipstream_effects_flag, propDia_flag,
266 Throttle_pct_input_flag, forcemom_flag, Xp_input_flag, Zp_input_flag, Mp_input_flag};
268 // CD ========= Aerodynamic x-force quantities (longitudinal)
269 // added to uiuc_map_CD.cpp
270 enum {CDo_flag = 8000, CDK_flag, CLK_flag, CD_a_flag, CD_adot_flag, CD_q_flag, CD_ih_flag,
271 CD_de_flag, CD_dr_flag, CD_da_flag, CD_beta_flag,
275 CDfa_flag, CDfCL_flag, CDfade_flag, CDfdf_flag, CDfadf_flag,
276 CXo_flag, CXK_flag, CX_a_flag, CX_a2_flag, CX_a3_flag, CX_adot_flag,
277 CX_q_flag, CX_de_flag, CX_dr_flag, CX_df_flag, CX_adf_flag,
278 CXfabetaf_flag, CXfadef_flag, CXfaqf_flag};
280 // CL ========= Aerodynamic z-force quantities (longitudinal)
281 // added to uiuc_map_CL.cpp
282 enum {CLo_flag = 9000, CL_a_flag, CL_adot_flag, CL_q_flag, CL_ih_flag, CL_de_flag,
286 CLfa_flag, CLfade_flag, CLfdf_flag, CLfadf_flag,
287 CZo_flag, CZ_a_flag, CZ_a2_flag, CZ_a3_flag, CZ_adot_flag,
288 CZ_q_flag, CZ_de_flag, CZ_deb2_flag, CZ_df_flag, CZ_adf_flag,
289 CZfa_flag, CZfabetaf_flag, CZfadef_flag, CZfaqf_flag};
291 // Cm ========= Aerodynamic m-moment quantities (longitudinal)
292 // added to uiuc_map_Cm.cpp
293 enum {Cmo_flag = 10000, Cm_a_flag, Cm_a2_flag, Cm_adot_flag, Cm_q_flag,
294 Cm_ih_flag, Cm_de_flag, Cm_b2_flag, Cm_r_flag,
298 Cmfa_flag, Cmfade_flag, Cmfdf_flag, Cmfadf_flag,
299 Cmfabetaf_flag, Cmfadef_flag, Cmfaqf_flag};
301 // CY ========= Aerodynamic y-force quantities (lateral)
302 // added to uiuc_map_CY.cpp
303 enum {CYo_flag = 11000, CY_beta_flag, CY_p_flag, CY_r_flag, CY_da_flag,
304 CY_dr_flag, CY_dra_flag, CY_bdot_flag, CYfada_flag, CYfbetadr_flag,
305 CYfabetaf_flag, CYfadaf_flag, CYfadrf_flag, CYfapf_flag, CYfarf_flag};
307 // Cl ========= Aerodynamic l-moment quantities (lateral)
308 // added to uiuc_map_Cl.cpp
309 enum {Clo_flag = 12000, Cl_beta_flag, Cl_p_flag, Cl_r_flag, Cl_da_flag,
310 Cl_dr_flag, Cl_daa_flag, Clfada_flag, Clfbetadr_flag, Clfabetaf_flag,
311 Clfadaf_flag, Clfadrf_flag, Clfapf_flag, Clfarf_flag};
313 // Cn ========= Aerodynamic n-moment quantities (lateral)
314 // added to uiuc_map_Cn.cpp
315 enum {Cno_flag = 13000, Cn_beta_flag, Cn_p_flag, Cn_r_flag, Cn_da_flag,
316 Cn_dr_flag, Cn_q_flag, Cn_b3_flag, Cnfada_flag, Cnfbetadr_flag,
317 Cnfabetaf_flag, Cnfadaf_flag, Cnfadrf_flag, Cnfapf_flag, Cnfarf_flag};
319 // gear ======= Landing gear model quantities
320 // added to uiuc_map_gear.cpp
321 enum {Dx_gear_flag = 14000, Dy_gear_flag, Dz_gear_flag, cgear_flag,
322 kgear_flag, muGear_flag, strutLength_flag,
323 gear_max_flag, gear_rate_flag, use_gear_flag};
325 // ice ======== Ice model quantities
326 // added to uiuc_map_ice.cpp
327 enum {iceTime_flag = 15000, transientTime_flag, eta_ice_final_flag,
328 beta_probe_wing_flag, beta_probe_tail_flag,
329 kCDo_flag, kCDK_flag, kCD_a_flag, kCD_adot_flag, kCD_q_flag, kCD_de_flag,
330 kCXo_flag, kCXK_flag, kCX_a_flag, kCX_a2_flag, kCX_a3_flag, kCX_adot_flag,
331 kCX_q_flag, kCX_de_flag, kCX_dr_flag, kCX_df_flag, kCX_adf_flag,
332 kCLo_flag, kCL_a_flag, kCL_adot_flag, kCL_q_flag, kCL_de_flag,
333 kCZo_flag, kCZ_a_flag, kCZ_a2_flag, kCZ_a3_flag, kCZ_adot_flag,
334 kCZ_q_flag, kCZ_de_flag, kCZ_deb2_flag, kCZ_df_flag, kCZ_adf_flag,
335 kCmo_flag, kCm_a_flag, kCm_a2_flag, kCm_adot_flag, kCm_q_flag,
336 kCm_de_flag, kCm_b2_flag, kCm_r_flag, kCm_df_flag,
337 kCYo_flag, kCY_beta_flag, kCY_p_flag, kCY_r_flag, kCY_da_flag,
338 kCY_dr_flag, kCY_dra_flag, kCY_bdot_flag,
339 kClo_flag, kCl_beta_flag, kCl_p_flag, kCl_r_flag, kCl_da_flag,
340 kCl_dr_flag, kCl_daa_flag,
341 kCno_flag, kCn_beta_flag, kCn_p_flag, kCn_r_flag, kCn_da_flag,
342 kCn_dr_flag, kCn_q_flag, kCn_b3_flag, bootTime_flag,
344 eta_wing_left_input_flag, eta_wing_right_input_flag,
345 eta_tail_input_flag, nonlin_ice_case_flag, eta_tail_flag,
346 eta_wing_left_flag, eta_wing_right_flag,
348 demo_eps_alpha_max_flag, demo_eps_pitch_max_flag,
349 demo_eps_pitch_min_flag, demo_eps_roll_max_flag,
350 demo_eps_thrust_min_flag, demo_eps_flap_max_flag,
351 demo_eps_airspeed_max_flag, demo_eps_airspeed_min_flag,
352 demo_boot_cycle_tail_flag, demo_boot_cycle_wing_left_flag,
353 demo_boot_cycle_wing_right_flag, demo_eps_pitch_input_flag,
354 tactilefadef_flag, tactile_pitch_flag, demo_ap_pah_on_flag,
355 demo_ap_alh_on_flag, demo_ap_rah_on_flag, demo_ap_hh_on_flag,
356 demo_ap_Theta_ref_flag, demo_ap_alt_ref_flag,
357 demo_ap_Phi_ref_flag, demo_ap_Psi_ref_flag,
358 demo_tactile_flag, demo_ice_tail_flag,
359 demo_ice_left_flag, demo_ice_right_flag};
361 // record ===== Record desired quantites to file
362 enum {Simtime_record = 16000, dt_record,
364 cbar_2U_record, b_2U_record, ch_2U_record,
366 // added to uiuc_map_record1.cpp
367 Weight_record, Mass_record, I_xx_record, I_yy_record, I_zz_record, I_xz_record,
368 Mass_appMass_ratio_record, I_xx_appMass_ratio_record,
369 I_yy_appMass_ratio_record, I_zz_appMass_ratio_record,
370 Mass_appMass_record, I_xx_appMass_record,
371 I_yy_appMass_record, I_zz_appMass_record,
373 // added to uiuc_map_record1.cpp
374 Dx_pilot_record, Dy_pilot_record, Dz_pilot_record,
375 Dx_cg_record, Dy_cg_record, Dz_cg_record,
376 Lat_geocentric_record, Lon_geocentric_record, Radius_to_vehicle_record,
377 Latitude_record, Longitude_record, Altitude_record,
378 Phi_record, Theta_record, Psi_record,
379 Phi_deg_record, Theta_deg_record, Psi_deg_record,
381 // added to uiuc_map_record1.cpp
382 V_dot_north_record, V_dot_east_record, V_dot_down_record,
383 U_dot_body_record, V_dot_body_record, W_dot_body_record,
384 A_X_pilot_record, A_Y_pilot_record, A_Z_pilot_record,
385 A_X_cg_record, A_Y_cg_record, A_Z_cg_record,
386 N_X_pilot_record, N_Y_pilot_record, N_Z_pilot_record,
387 N_X_cg_record, N_Y_cg_record, N_Z_cg_record,
388 P_dot_body_record, Q_dot_body_record, R_dot_body_record,
390 // added to uiuc_map_record2.cpp
391 V_north_record, V_east_record, V_down_record,
392 V_north_rel_ground_record, V_east_rel_ground_record, V_down_rel_ground_record,
393 V_north_airmass_record, V_east_airmass_record, V_down_airmass_record,
394 V_north_rel_airmass_record, V_east_rel_airmass_record, V_down_rel_airmass_record,
395 U_gust_record, V_gust_record, W_gust_record,
396 U_body_record, V_body_record, W_body_record,
397 V_rel_wind_record, V_true_kts_record, V_rel_ground_record,
398 V_inertial_record, V_ground_speed_record, V_equiv_record,
399 V_equiv_kts_record, V_calibrated_record, V_calibrated_kts_record,
400 P_local_record, Q_local_record, R_local_record,
401 P_body_record, Q_body_record, R_body_record,
402 P_total_record, Q_total_record, R_total_record,
403 Phi_dot_record, Theta_dot_record, Psi_dot_record,
404 Latitude_dot_record, Longitude_dot_record, Radius_dot_record,
406 // added to uiuc_map_record2.cpp
407 Alpha_record, Alpha_deg_record, Alpha_dot_record, Alpha_dot_deg_record,
408 Beta_record, Beta_deg_record, Beta_dot_record, Beta_dot_deg_record,
409 Gamma_vert_record, Gamma_vert_deg_record, Gamma_horiz_record, Gamma_horiz_deg_record,
411 // added to uiuc_map_record3.cpp
412 Density_record, V_sound_record, Mach_number_record,
413 Static_pressure_record, Total_pressure_record, Impact_pressure_record,
414 Dynamic_pressure_record,
415 Static_temperature_record, Total_temperature_record,
417 // added to uiuc_map_record3.cpp
418 Gravity_record, Sea_level_radius_record, Earth_position_angle_record,
419 Runway_altitude_record, Runway_latitude_record, Runway_longitude_record,
420 Runway_heading_record, Radius_to_rwy_record,
421 D_pilot_north_of_rwy_record, D_pilot_east_of_rwy_record, D_pilot_above_rwy_record,
422 X_pilot_rwy_record, Y_pilot_rwy_record, H_pilot_rwy_record,
423 D_cg_north_of_rwy_record, D_cg_east_of_rwy_record, D_cg_above_rwy_record,
424 X_cg_rwy_record, Y_cg_rwy_record, H_cg_rwy_record,
426 // added to uiuc_map_record3.cpp
427 Throttle_3_record, Throttle_pct_record,
429 // added to uiuc_map_record3.cpp
430 Long_control_record, Long_trim_record, Long_trim_deg_record,
431 elevator_record, elevator_deg_record,
432 Lat_control_record, aileron_record, aileron_deg_record,
433 Rudder_pedal_record, rudder_record, rudder_deg_record,
434 Flap_handle_record, flap_cmd_record, flap_cmd_deg_record,
435 flap_pos_record, flap_pos_deg_record, flap_pos_norm_record,
436 Spoiler_handle_record, spoiler_cmd_deg_record,
437 spoiler_pos_deg_record, spoiler_pos_norm_record, spoiler_pos_record,
440 // added to uiuc_map_record4.cpp
441 CD_record, CDfaI_record, CDfCLI_record, CDfadeI_record, CDfdfI_record,
442 CDfadfI_record, CX_record, CXfabetafI_record, CXfadefI_record,
444 CDo_save_record, CDK_save_record, CLK_save_record, CD_a_save_record, CD_adot_save_record,
445 CD_q_save_record, CD_ih_save_record,
446 CD_de_save_record, CD_dr_save_record, CD_da_save_record, CD_beta_save_record,
451 CXK_save_record, CX_a_save_record, CX_a2_save_record, CX_a3_save_record,
452 CX_adot_save_record, CX_q_save_record, CX_de_save_record,
453 CX_dr_save_record, CX_df_save_record, CX_adf_save_record,
454 CL_record, CLfaI_record, CLfadeI_record, CLfdfI_record, CLfadfI_record,
455 CZ_record, CZfaI_record, CZfabetafI_record, CZfadefI_record,
457 CLo_save_record, CL_a_save_record, CL_adot_save_record, CL_q_save_record,
458 CL_ih_save_record, CL_de_save_record,
462 CZo_save_record, CZ_a_save_record,
463 CZ_a2_save_record, CZ_a3_save_record, CZ_adot_save_record,
464 CZ_q_save_record, CZ_de_save_record, CZ_deb2_save_record,
465 CZ_df_save_record, CZ_adf_save_record,
466 Cm_record, CmfaI_record, CmfadeI_record, CmfdfI_record, CmfadfI_record,
467 CmfabetafI_record, CmfadefI_record, CmfaqfI_record,
468 Cmo_save_record, Cm_a_save_record, Cm_a2_save_record,
469 Cm_adot_save_record, Cm_q_save_record, Cm_ih_save_record,
470 Cm_de_save_record, Cm_b2_save_record, Cm_r_save_record,
474 CY_record, CYfadaI_record, CYfbetadrI_record, CYfabetafI_record,
475 CYfadafI_record, CYfadrfI_record, CYfapfI_record, CYfarfI_record,
476 CYo_save_record, CY_beta_save_record, CY_p_save_record,
477 CY_r_save_record, CY_da_save_record, CY_dr_save_record,
478 CY_dra_save_record, CY_bdot_save_record,
479 Cl_record, ClfadaI_record, ClfbetadrI_record, ClfabetafI_record,
480 ClfadafI_record, ClfadrfI_record, ClfapfI_record, ClfarfI_record,
481 Clo_save_record, Cl_beta_save_record, Cl_p_save_record, Cl_r_save_record,
482 Cl_da_save_record, Cl_dr_save_record, Cl_daa_save_record,
483 Cn_record, CnfadaI_record, CnfbetadrI_record, CnfabetafI_record,
484 CnfadafI_record, CnfadrfI_record, CnfapfI_record, CnfarfI_record,
485 Cno_save_record, Cn_beta_save_record, Cn_p_save_record, Cn_r_save_record,
486 Cn_da_save_record, Cn_dr_save_record, Cn_q_save_record,
489 // added to uiuc_map_record5.cpp
490 F_X_wind_record, F_Y_wind_record, F_Z_wind_record,
491 F_X_aero_record, F_Y_aero_record, F_Z_aero_record,
492 F_X_engine_record, F_Y_engine_record, F_Z_engine_record,
493 F_X_gear_record, F_Y_gear_record, F_Z_gear_record,
494 F_X_record, F_Y_record, F_Z_record,
495 F_north_record, F_east_record, F_down_record,
497 // added to uiuc_map_record5.cpp
498 M_l_aero_record, M_m_aero_record, M_n_aero_record,
499 M_l_engine_record, M_m_engine_record, M_n_engine_record,
500 M_l_gear_record, M_m_gear_record, M_n_gear_record,
501 M_l_rp_record, M_m_rp_record, M_n_rp_record,
502 M_l_cg_record, M_m_cg_record, M_n_cg_record,
504 // added to uiuc_map_record5.cpp
505 flapper_freq_record, flapper_phi_record,
506 flapper_phi_deg_record, flapper_Lift_record, flapper_Thrust_record,
507 flapper_Inertia_record, flapper_Moment_record,
509 // added to uiuc_map_record5.cpp
516 elevator_sas_deg_record,
517 aileron_sas_deg_record,
518 rudder_sas_deg_record,
520 downwashAngle_deg_record,
521 alphaTail_deg_record,
528 // added to uiuc_map_record5.cpp
529 Gear_handle_record, gear_cmd_norm_record, gear_pos_norm_record,
531 // added to uiuc_map_record5.cpp
540 // added to uiuc_map_record6.cpp
541 CL_clean_record, CL_iced_record,
542 CD_clean_record, CD_iced_record,
543 Cm_clean_record, Cm_iced_record,
544 Ch_clean_record, Ch_iced_record,
545 Cl_clean_record, Cl_iced_record,
546 Cn_clean_record, Cn_iced_record,
547 CLclean_wing_record, CLiced_wing_record,
548 CLclean_tail_record, CLiced_tail_record,
549 Lift_clean_wing_record, Lift_iced_wing_record,
550 Lift_clean_tail_record, Lift_iced_tail_record,
551 Gamma_clean_wing_record, Gamma_iced_wing_record,
552 Gamma_clean_tail_record, Gamma_iced_tail_record,
553 w_clean_wing_record, w_iced_wing_record,
554 w_clean_tail_record, w_iced_tail_record,
555 V_total_clean_wing_record, V_total_iced_wing_record,
556 V_total_clean_tail_record, V_total_iced_tail_record,
557 beta_flow_clean_wing_record, beta_flow_clean_wing_deg_record,
558 beta_flow_iced_wing_record, beta_flow_iced_wing_deg_record,
559 beta_flow_clean_tail_record, beta_flow_clean_tail_deg_record,
560 beta_flow_iced_tail_record, beta_flow_iced_tail_deg_record,
561 Dbeta_flow_wing_record, Dbeta_flow_wing_deg_record,
562 Dbeta_flow_tail_record, Dbeta_flow_tail_deg_record,
563 pct_beta_flow_wing_record, pct_beta_flow_tail_record, eta_ice_record,
564 eta_wing_right_record, eta_wing_left_record, eta_tail_record,
565 delta_CL_record, delta_CD_record, delta_Cm_record, delta_Cl_record,
568 // added to uiuc_map_record6.cpp
569 boot_cycle_tail_record, boot_cycle_wing_left_record,
570 boot_cycle_wing_right_record, autoIPS_tail_record,
571 autoIPS_wing_left_record, autoIPS_wing_right_record,
572 eps_pitch_input_record, eps_alpha_max_record, eps_pitch_max_record,
573 eps_pitch_min_record, eps_roll_max_record, eps_thrust_min_record,
574 eps_flap_max_record, eps_airspeed_max_record, eps_airspeed_min_record,
575 tactilefadefI_record,
577 // added to uiuc_map_record6.cpp
578 ap_pah_on_record, ap_alh_on_record, ap_Theta_ref_deg_record,
579 ap_Theta_ref_rad_record, ap_alt_ref_ft_record, trigger_on_record,
580 ap_rah_on_record, ap_Phi_ref_rad_record, ap_Phi_ref_deg_record,
581 ap_hh_on_record, ap_Psi_ref_rad_record, ap_Psi_ref_deg_record,
582 trigger_num_record, trigger_toggle_record, trigger_counter_record,
584 // added to uiuc_map_record6.cpp
585 T_local_to_body_11_record, T_local_to_body_12_record,
586 T_local_to_body_13_record, T_local_to_body_21_record,
587 T_local_to_body_22_record, T_local_to_body_23_record,
588 T_local_to_body_31_record, T_local_to_body_32_record,
589 T_local_to_body_33_record};
592 // misc ======= Miscellaneous inputs
593 // added to uiuc_map_misc.cpp
594 enum {simpleHingeMomentCoef_flag = 17000, flapper_flag,
595 flapper_phi_init_flag};
598 // fog ======== Fog field quantities
599 enum {fog_segments_flag = 18000, fog_point_flag};
604 // ParseFile stuff [] Bipin to add more comments
606 #define airplane aircraft_->airplane
607 ParseFile *initParts;
608 #define initParts aircraft_->initParts
609 ParseFile *geometryParts;
610 #define geometryParts aircraft_->geometryParts
611 ParseFile *massParts;
612 #define massParts aircraft_->massParts
613 ParseFile *aeroDragParts;
614 #define aeroDragParts aircraft_->aeroDragParts
615 ParseFile *aeroLiftParts;
616 #define aeroLiftParts aircraft_->aeroLiftParts
617 ParseFile *aeroPitchParts;
618 #define aeroPitchParts aircraft_->aeroPitchParts
619 ParseFile *aeroSideforceParts;
620 #define aeroSideforceParts aircraft_->aeroSideforceParts
621 ParseFile *aeroRollParts;
622 #define aeroRollParts aircraft_->aeroRollParts
623 ParseFile *aeroYawParts;
624 #define aeroYawParts aircraft_->aeroYawParts
625 ParseFile *engineParts;
626 #define engineParts aircraft_->engineParts
627 ParseFile *gearParts;
628 #define gearParts aircraft_->gearParts
629 ParseFile *recordParts;
630 #define recordParts aircraft_->recordParts
632 /*= Keywords (token1) ===========================================*/
633 std::map <string,int> Keyword_map;
634 #define Keyword_map aircraft_->Keyword_map
636 double CD, CX, CL, CZ, Cm, CY, Cl, Cn;
637 #define CD aircraft_->CD
638 #define CX aircraft_->CX
639 #define CL aircraft_->CL
640 #define CZ aircraft_->CZ
641 #define Cm aircraft_->Cm
642 #define CY aircraft_->CY
643 #define Cl aircraft_->Cl
644 #define Cn aircraft_->Cn
645 double CXclean_wing, CXclean_tail, CXiced_wing, CXiced_tail;
646 double CLclean_wing, CLclean_tail, CLiced_wing, CLiced_tail;
647 double CZclean_wing, CZclean_tail, CZiced_wing, CZiced_tail;
648 #define CXclean_wing aircraft_->CXclean_wing
649 #define CXclean_tail aircraft_->CXclean_tail
650 #define CXiced_wing aircraft_->CXiced_wing
651 #define CXiced_tail aircraft_->CXiced_tail
652 #define CLclean_wing aircraft_->CLclean_wing
653 #define CLclean_tail aircraft_->CLclean_tail
654 #define CLiced_wing aircraft_->CLiced_wing
655 #define CLiced_tail aircraft_->CLiced_tail
656 #define CZclean_wing aircraft_->CZclean_wing
657 #define CZclean_tail aircraft_->CZclean_tail
658 #define CZiced_wing aircraft_->CZiced_wing
659 #define CZiced_tail aircraft_->CZiced_tail
661 /*========================================*/
662 /* Variables (token2) - 17 groups (000329)*/
663 /*========================================*/
665 /* Variables (token2) ===========================================*/
666 /* init ========== Initial values for equations of motion =======*/
668 std::map <string,int> init_map;
669 #define init_map aircraft_->init_map
672 #define recordRate aircraft_->recordRate
673 double recordStartTime;
674 #define recordStartTime aircraft_->recordStartTime
675 bool use_V_rel_wind_2U;
676 #define use_V_rel_wind_2U aircraft_->use_V_rel_wind_2U
677 bool nondim_rate_V_rel_wind;
678 #define nondim_rate_V_rel_wind aircraft_->nondim_rate_V_rel_wind
679 bool use_abs_U_body_2U;
680 #define use_abs_U_body_2U aircraft_->use_abs_U_body_2U
682 #define dyn_on_speed aircraft_->dyn_on_speed
683 double dyn_on_speed_zero;
684 #define dyn_on_speed_zero aircraft_->dyn_on_speed_zero
685 bool use_dyn_on_speed_curve1;
686 #define use_dyn_on_speed_curve1 aircraft_->use_dyn_on_speed_curve1
688 bool use_Alpha_dot_on_speed;
689 #define use_Alpha_dot_on_speed aircraft_->use_Alpha_dot_on_speed
690 double Alpha_dot_on_speed;
691 #define Alpha_dot_on_speed aircraft_->Alpha_dot_on_speed
693 bool use_gamma_horiz_on_speed;
694 #define use_gamma_horiz_on_speed aircraft_->use_gamma_horiz_on_speed
695 double gamma_horiz_on_speed;
696 #define gamma_horiz_on_speed aircraft_->gamma_horiz_on_speed
700 #define b_downwashMode aircraft_->b_downwashMode
702 #define downwashMode aircraft_->downwashMode
704 #define downwashCoef aircraft_->downwashCoef
706 #define gammaWing aircraft_->gammaWing
708 #define downwash aircraft_->downwash
709 double downwashAngle;
710 #define downwashAngle aircraft_->downwashAngle
712 #define alphaTail aircraft_->alphaTail
715 bool P_body_init_true;
717 #define P_body_init_true aircraft_->P_body_init_true
718 #define P_body_init aircraft_->P_body_init
719 bool Q_body_init_true;
721 #define Q_body_init_true aircraft_->Q_body_init_true
722 #define Q_body_init aircraft_->Q_body_init
723 bool R_body_init_true;
725 #define R_body_init_true aircraft_->R_body_init_true
726 #define R_body_init aircraft_->R_body_init
729 #define Phi_init_true aircraft_->Phi_init_true
730 #define Phi_init aircraft_->Phi_init
731 bool Theta_init_true;
733 #define Theta_init_true aircraft_->Theta_init_true
734 #define Theta_init aircraft_->Theta_init
737 #define Psi_init_true aircraft_->Psi_init_true
738 #define Psi_init aircraft_->Psi_init
739 bool Alpha_init_true;
741 #define Alpha_init_true aircraft_->Alpha_init_true
742 #define Alpha_init aircraft_->Alpha_init
745 #define Beta_init_true aircraft_->Beta_init_true
746 #define Beta_init aircraft_->Beta_init
747 bool U_body_init_true;
749 #define U_body_init_true aircraft_->U_body_init_true
750 #define U_body_init aircraft_->U_body_init
751 bool V_body_init_true;
753 #define V_body_init_true aircraft_->V_body_init_true
754 #define V_body_init aircraft_->V_body_init
755 bool W_body_init_true;
757 #define W_body_init_true aircraft_->W_body_init_true
758 #define W_body_init aircraft_->W_body_init
760 #define trim_case_2 aircraft_->trim_case_2
761 bool use_uiuc_network;
764 #define use_uiuc_network aircraft_->use_uiuc_network
765 #define server_IP aircraft_->server_IP
766 #define port_num aircraft_->port_num
768 #define icing_demo aircraft_->icing_demo
769 bool outside_control;
770 #define outside_control aircraft_->outside_control
772 /* Variables (token2) ===========================================*/
773 /* geometry ====== Aircraft-specific geometric quantities =======*/
775 std::map <string,int> geometry_map;
776 #define geometry_map aircraft_->geometry_map
778 double bw, cbar, Sw, ih, bh, chord_h, Sh;
779 #define bw aircraft_->bw
780 #define cbar aircraft_->cbar
781 #define Sw aircraft_->Sw
782 #define ih aircraft_->ih
783 #define bh aircraft_->bh
784 #define chord_h aircraft_->chord_h
785 #define Sh aircraft_->Sh
788 /* Variables (token2) ===========================================*/
789 /* controlSurface Control surface deflections and properties ===*/
791 std::map <string,int> controlSurface_map;
792 #define controlSurface_map aircraft_->controlSurface_map
797 #define demax aircraft_->demax
798 #define demin aircraft_->demin
799 #define damax aircraft_->damax
800 #define damin aircraft_->damin
801 #define drmax aircraft_->drmax
802 #define drmin aircraft_->drmin
804 double aileron, elevator, rudder;
805 #define aileron aircraft_->aileron
806 #define elevator aircraft_->elevator
807 #define rudder aircraft_->rudder
809 //#define flap aircraft_->flap
811 bool set_Long_trim, zero_Long_trim;
812 double Long_trim_constant;
813 #define set_Long_trim aircraft_->set_Long_trim
814 #define Long_trim_constant aircraft_->Long_trim_constant
815 #define zero_Long_trim aircraft_->zero_Long_trim
818 double elevator_step_angle, elevator_step_startTime;
819 #define elevator_step aircraft_->elevator_step
820 #define elevator_step_angle aircraft_->elevator_step_angle
821 #define elevator_step_startTime aircraft_->elevator_step_startTime
823 bool elevator_singlet;
824 double elevator_singlet_angle, elevator_singlet_startTime;
825 double elevator_singlet_duration;
826 #define elevator_singlet aircraft_->elevator_singlet
827 #define elevator_singlet_angle aircraft_->elevator_singlet_angle
828 #define elevator_singlet_startTime aircraft_->elevator_singlet_startTime
829 #define elevator_singlet_duration aircraft_->elevator_singlet_duration
831 bool elevator_doublet;
832 double elevator_doublet_angle, elevator_doublet_startTime;
833 double elevator_doublet_duration;
834 #define elevator_doublet aircraft_->elevator_doublet
835 #define elevator_doublet_angle aircraft_->elevator_doublet_angle
836 #define elevator_doublet_startTime aircraft_->elevator_doublet_startTime
837 #define elevator_doublet_duration aircraft_->elevator_doublet_duration
840 string elevator_input_file;
841 double elevator_input_timeArray[7500];
842 double elevator_input_deArray[7500];
843 int elevator_input_ntime;
844 double elevator_input_startTime;
845 #define elevator_input aircraft_->elevator_input
846 #define elevator_input_file aircraft_->elevator_input_file
847 #define elevator_input_timeArray aircraft_->elevator_input_timeArray
848 #define elevator_input_deArray aircraft_->elevator_input_deArray
849 #define elevator_input_ntime aircraft_->elevator_input_ntime
850 #define elevator_input_startTime aircraft_->elevator_input_startTime
853 string aileron_input_file;
854 double aileron_input_timeArray[1500];
855 double aileron_input_daArray[1500];
856 int aileron_input_ntime;
857 double aileron_input_startTime;
858 #define aileron_input aircraft_->aileron_input
859 #define aileron_input_file aircraft_->aileron_input_file
860 #define aileron_input_timeArray aircraft_->aileron_input_timeArray
861 #define aileron_input_daArray aircraft_->aileron_input_daArray
862 #define aileron_input_ntime aircraft_->aileron_input_ntime
863 #define aileron_input_startTime aircraft_->aileron_input_startTime
866 string rudder_input_file;
867 double rudder_input_timeArray[500];
868 double rudder_input_drArray[500];
869 int rudder_input_ntime;
870 double rudder_input_startTime;
871 #define rudder_input aircraft_->rudder_input
872 #define rudder_input_file aircraft_->rudder_input_file
873 #define rudder_input_timeArray aircraft_->rudder_input_timeArray
874 #define rudder_input_drArray aircraft_->rudder_input_drArray
875 #define rudder_input_ntime aircraft_->rudder_input_ntime
876 #define rudder_input_startTime aircraft_->rudder_input_startTime
879 #define pilot_elev_no aircraft_->pilot_elev_no
880 bool pilot_elev_no_check;
881 #define pilot_elev_no_check aircraft_->pilot_elev_no_check
884 #define pilot_ail_no aircraft_->pilot_ail_no
885 bool pilot_ail_no_check;
886 #define pilot_ail_no_check aircraft_->pilot_ail_no_check
889 #define pilot_rud_no aircraft_->pilot_rud_no
890 bool pilot_rud_no_check;
891 #define pilot_rud_no_check aircraft_->pilot_rud_no_check
893 double flap_max, flap_rate;
894 #define flap_max aircraft_->flap_max
895 #define flap_rate aircraft_->flap_rate
897 #define use_flaps aircraft_->use_flaps
899 double spoiler_max, spoiler_rate;
900 #define spoiler_max aircraft_->spoiler_max
901 #define spoiler_rate aircraft_->spoiler_rate
903 #define use_spoilers aircraft_->use_spoilers
907 string flap_pos_input_file;
908 double flap_pos_input_timeArray[500];
909 double flap_pos_input_dfArray[500];
910 int flap_pos_input_ntime;
911 double flap_pos_input_startTime;
912 #define flap_pos_input aircraft_->flap_pos_input
913 #define flap_pos_input_file aircraft_->flap_pos_input_file
914 #define flap_pos_input_timeArray aircraft_->flap_pos_input_timeArray
915 #define flap_pos_input_dfArray aircraft_->flap_pos_input_dfArray
916 #define flap_pos_input_ntime aircraft_->flap_pos_input_ntime
917 #define flap_pos_input_startTime aircraft_->flap_pos_input_startTime
920 // SAS system: pitch, roll and yaw damping MSS
921 double elevator_sas_KQ;
922 double elevator_sas_max;
923 double elevator_sas_min;
924 double elevator_stick_gain;
925 double aileron_sas_KP;
926 double aileron_sas_max;
927 double aileron_stick_gain;
928 double rudder_sas_KR;
929 double rudder_sas_max;
930 double rudder_stick_gain;
934 #define elevator_sas_KQ aircraft_->elevator_sas_KQ
935 #define elevator_sas_max aircraft_->elevator_sas_max
936 #define elevator_sas_min aircraft_->elevator_sas_min
937 #define elevator_stick_gain aircraft_->elevator_stick_gain
938 #define aileron_sas_KP aircraft_->aileron_sas_KP
939 #define aileron_sas_max aircraft_->aileron_sas_max
940 #define aileron_stick_gain aircraft_->aileron_stick_gain
941 #define rudder_sas_KR aircraft_->rudder_sas_KR
942 #define rudder_sas_max aircraft_->rudder_sas_max
943 #define rudder_stick_gain aircraft_->rudder_stick_gain
946 #define elevator_sas aircraft_->elevator_sas
948 #define aileron_sas aircraft_->aileron_sas
950 #define rudder_sas aircraft_->rudder_sas
952 bool use_elevator_sas_type1;
953 #define use_elevator_sas_type1 aircraft_->use_elevator_sas_type1
954 bool use_elevator_sas_max;
955 #define use_elevator_sas_max aircraft_->use_elevator_sas_max
956 bool use_elevator_sas_min;
957 #define use_elevator_sas_min aircraft_->use_elevator_sas_min
958 bool use_elevator_stick_gain;
959 #define use_elevator_stick_gain aircraft_->use_elevator_stick_gain
960 bool use_aileron_sas_type1;
961 #define use_aileron_sas_type1 aircraft_->use_aileron_sas_type1
962 bool use_aileron_sas_max;
963 #define use_aileron_sas_max aircraft_->use_aileron_sas_max
964 bool use_aileron_stick_gain;
965 #define use_aileron_stick_gain aircraft_->use_aileron_stick_gain
966 bool use_rudder_sas_type1;
967 #define use_rudder_sas_type1 aircraft_->use_rudder_sas_type1
968 bool use_rudder_sas_max;
969 #define use_rudder_sas_max aircraft_->use_rudder_sas_max
970 bool use_rudder_stick_gain;
971 #define use_rudder_stick_gain aircraft_->use_rudder_stick_gain
975 /* Variables (token2) ===========================================*/
976 /* controlsMixer = Control mixer ================================*/
978 std::map <string,int> controlsMixer_map;
979 #define controlsMixer_map aircraft_->controlsMixer_map
982 #define nomix aircraft_->nomix
985 /* Variables (token2) ===========================================*/
986 /* mass =========== Aircraft-specific mass properties ===========*/
988 std::map <string,int> mass_map;
989 #define mass_map aircraft_->mass_map
992 #define Weight aircraft_->Weight
994 double Mass_appMass_ratio;
995 #define Mass_appMass_ratio aircraft_->Mass_appMass_ratio
996 double I_xx_appMass_ratio;
997 #define I_xx_appMass_ratio aircraft_->I_xx_appMass_ratio
998 double I_yy_appMass_ratio;
999 #define I_yy_appMass_ratio aircraft_->I_yy_appMass_ratio
1000 double I_zz_appMass_ratio;
1001 #define I_zz_appMass_ratio aircraft_->I_zz_appMass_ratio
1002 double Mass_appMass;
1003 #define Mass_appMass aircraft_->Mass_appMass
1004 double I_xx_appMass;
1005 #define I_xx_appMass aircraft_->I_xx_appMass
1006 double I_yy_appMass;
1007 #define I_yy_appMass aircraft_->I_yy_appMass
1008 double I_zz_appMass;
1009 #define I_zz_appMass aircraft_->I_zz_appMass
1011 /* Variables (token2) ===========================================*/
1012 /* engine ======== Propulsion data ==============================*/
1014 std::map <string,int> engine_map;
1015 #define engine_map aircraft_->engine_map
1017 double simpleSingleMaxThrust;
1018 #define simpleSingleMaxThrust aircraft_->simpleSingleMaxThrust
1020 bool simpleSingleModel;
1021 #define simpleSingleModel aircraft_->simpleSingleModel
1023 #define t_v0 aircraft_->t_v0
1025 #define dtdv_t0 aircraft_->dtdv_t0
1027 #define v_t0 aircraft_->v_t0
1029 #define dtdvvt aircraft_->dtdvvt
1031 double tc, induced, eta_q;
1032 #define tc aircraft_->tc
1033 #define induced aircraft_->induced
1034 #define eta_q aircraft_->eta_q
1036 bool Throttle_pct_input;
1037 string Throttle_pct_input_file;
1038 double Throttle_pct_input_timeArray[1500];
1039 double Throttle_pct_input_dTArray[1500];
1040 int Throttle_pct_input_ntime;
1041 double Throttle_pct_input_startTime;
1042 #define Throttle_pct_input aircraft_->Throttle_pct_input
1043 #define Throttle_pct_input_file aircraft_->Throttle_pct_input_file
1044 #define Throttle_pct_input_timeArray aircraft_->Throttle_pct_input_timeArray
1045 #define Throttle_pct_input_dTArray aircraft_->Throttle_pct_input_dTArray
1046 #define Throttle_pct_input_ntime aircraft_->Throttle_pct_input_ntime
1047 #define Throttle_pct_input_startTime aircraft_->Throttle_pct_input_startTime
1048 bool gyroForce_Q_body, gyroForce_R_body;
1049 double minOmega, maxOmega, minOmegaRPM, maxOmegaRPM, engineOmega, polarInertia;
1050 #define gyroForce_Q_body aircraft_->gyroForce_Q_body
1051 #define gyroForce_R_body aircraft_->gyroForce_R_body
1052 #define minOmega aircraft_->minOmega
1053 #define maxOmega aircraft_->maxOmega
1054 #define minOmegaRPM aircraft_->minOmegaRPM
1055 #define maxOmegaRPM aircraft_->maxOmegaRPM
1056 #define engineOmega aircraft_->engineOmega
1057 #define polarInertia aircraft_->polarInertia
1059 // propeller slipstream effects
1060 bool b_slipstreamEffects;
1062 double eta_q_Cm_q, eta_q_Cm_q_fac;
1063 double eta_q_Cm_adot, eta_q_Cm_adot_fac;
1064 double eta_q_Cmfade, eta_q_Cmfade_fac;
1065 double eta_q_Cm_de, eta_q_Cm_de_fac;
1066 double eta_q_Cl_beta, eta_q_Cl_beta_fac;
1067 double eta_q_Cl_p, eta_q_Cl_p_fac;
1068 double eta_q_Cl_r, eta_q_Cl_r_fac;
1069 double eta_q_Cl_dr, eta_q_Cl_dr_fac;
1070 double eta_q_CY_beta, eta_q_CY_beta_fac;
1071 double eta_q_CY_p, eta_q_CY_p_fac;
1072 double eta_q_CY_r, eta_q_CY_r_fac;
1073 double eta_q_CY_dr, eta_q_CY_dr_fac;
1074 double eta_q_Cn_beta, eta_q_Cn_beta_fac;
1075 double eta_q_Cn_p, eta_q_Cn_p_fac;
1076 double eta_q_Cn_r, eta_q_Cn_r_fac;
1077 double eta_q_Cn_dr, eta_q_Cn_dr_fac;
1079 #define b_slipstreamEffects aircraft_->b_slipstreamEffects
1080 #define propDia aircraft_->propDia
1081 #define eta_q_Cm_q aircraft_->eta_q_Cm_q
1082 #define eta_q_Cm_q_fac aircraft_->eta_q_Cm_q_fac
1083 #define eta_q_Cm_adot aircraft_->eta_q_Cm_adot
1084 #define eta_q_Cm_adot_fac aircraft_->eta_q_Cm_adot_fac
1085 #define eta_q_Cmfade aircraft_->eta_q_Cmfade
1086 #define eta_q_Cmfade_fac aircraft_->eta_q_Cmfade_fac
1087 #define eta_q_Cm_de aircraft_->eta_q_Cm_de
1088 #define eta_q_Cm_de_fac aircraft_->eta_q_Cm_de_fac
1089 #define eta_q_Cl_beta aircraft_->eta_q_Cl_beta
1090 #define eta_q_Cl_beta_fac aircraft_->eta_q_Cl_beta_fac
1091 #define eta_q_Cl_p aircraft_->eta_q_Cl_p
1092 #define eta_q_Cl_p_fac aircraft_->eta_q_Cl_p_fac
1093 #define eta_q_Cl_r aircraft_->eta_q_Cl_r
1094 #define eta_q_Cl_r_fac aircraft_->eta_q_Cl_r_fac
1095 #define eta_q_Cl_dr aircraft_->eta_q_Cl_dr
1096 #define eta_q_Cl_dr_fac aircraft_->eta_q_Cl_dr_fac
1097 #define eta_q_CY_beta aircraft_->eta_q_CY_beta
1098 #define eta_q_CY_beta_fac aircraft_->eta_q_CY_beta_fac
1099 #define eta_q_CY_p aircraft_->eta_q_CY_p
1100 #define eta_q_CY_p_fac aircraft_->eta_q_CY_p_fac
1101 #define eta_q_CY_r aircraft_->eta_q_CY_r
1102 #define eta_q_CY_r_fac aircraft_->eta_q_CY_r_fac
1103 #define eta_q_CY_dr aircraft_->eta_q_CY_dr
1104 #define eta_q_CY_dr_fac aircraft_->eta_q_CY_dr_fac
1105 #define eta_q_Cn_beta aircraft_->eta_q_Cn_beta
1106 #define eta_q_Cn_beta_fac aircraft_->eta_q_Cn_beta_fac
1107 #define eta_q_Cn_p aircraft_->eta_q_Cn_p
1108 #define eta_q_Cn_p_fac aircraft_->eta_q_Cn_p_fac
1109 #define eta_q_Cn_r aircraft_->eta_q_Cn_r
1110 #define eta_q_Cn_r_fac aircraft_->eta_q_Cn_r_fac
1111 #define eta_q_Cn_dr aircraft_->eta_q_Cn_dr
1112 #define eta_q_Cn_dr_fac aircraft_->eta_q_Cn_dr_fac
1116 string Xp_input_file;
1117 double Xp_input_timeArray[5400];
1118 double Xp_input_XpArray[5400];
1120 double Xp_input_startTime;
1121 #define Xp_input aircraft_->Xp_input
1122 #define Xp_input_file aircraft_->Xp_input_file
1123 #define Xp_input_timeArray aircraft_->Xp_input_timeArray
1124 #define Xp_input_XpArray aircraft_->Xp_input_XpArray
1125 #define Xp_input_ntime aircraft_->Xp_input_ntime
1126 #define Xp_input_startTime aircraft_->Xp_input_startTime
1128 string Zp_input_file;
1129 double Zp_input_timeArray[5400];
1130 double Zp_input_ZpArray[5400];
1132 double Zp_input_startTime;
1133 #define Zp_input aircraft_->Zp_input
1134 #define Zp_input_file aircraft_->Zp_input_file
1135 #define Zp_input_timeArray aircraft_->Zp_input_timeArray
1136 #define Zp_input_ZpArray aircraft_->Zp_input_ZpArray
1137 #define Zp_input_ntime aircraft_->Zp_input_ntime
1138 #define Zp_input_startTime aircraft_->Zp_input_startTime
1140 string Mp_input_file;
1141 double Mp_input_timeArray[5400];
1142 double Mp_input_MpArray[5400];
1144 double Mp_input_startTime;
1145 #define Mp_input aircraft_->Mp_input
1146 #define Mp_input_file aircraft_->Mp_input_file
1147 #define Mp_input_timeArray aircraft_->Mp_input_timeArray
1148 #define Mp_input_MpArray aircraft_->Mp_input_MpArray
1149 #define Mp_input_ntime aircraft_->Mp_input_ntime
1150 #define Mp_input_startTime aircraft_->Mp_input_startTime
1153 /* Variables (token2) ===========================================*/
1154 /* CD ============ Aerodynamic x-force quantities (longitudinal) */
1156 std::map <string,int> CD_map;
1157 #define CD_map aircraft_->CD_map
1159 double CDo, CDK, CLK, CD_a, CD_adot, CD_q, CD_ih, CD_de, CD_dr, CD_da, CD_beta;
1160 double CD_df, CD_ds, CD_dg;
1161 #define CDo aircraft_->CDo
1162 #define CDK aircraft_->CDK
1163 #define CLK aircraft_->CLK
1164 #define CD_a aircraft_->CD_a
1165 #define CD_adot aircraft_->CD_adot
1166 #define CD_q aircraft_->CD_q
1167 #define CD_ih aircraft_->CD_ih
1168 #define CD_de aircraft_->CD_de
1169 #define CD_dr aircraft_->CD_dr
1170 #define CD_da aircraft_->CD_da
1171 #define CD_beta aircraft_->CD_beta
1172 #define CD_df aircraft_->CD_df
1173 #define CD_ds aircraft_->CD_ds
1174 #define CD_dg aircraft_->CD_dg
1176 #define b_CLK aircraft_->b_CLK
1178 double CDfa_aArray[100];
1179 double CDfa_CDArray[100];
1182 #define CDfa aircraft_->CDfa
1183 #define CDfa_aArray aircraft_->CDfa_aArray
1184 #define CDfa_CDArray aircraft_->CDfa_CDArray
1185 #define CDfa_nAlpha aircraft_->CDfa_nAlpha
1186 #define CDfaI aircraft_->CDfaI
1188 double CDfCL_CLArray[100];
1189 double CDfCL_CDArray[100];
1192 #define CDfCL aircraft_->CDfCL
1193 #define CDfCL_CLArray aircraft_->CDfCL_CLArray
1194 #define CDfCL_CDArray aircraft_->CDfCL_CDArray
1195 #define CDfCL_nCL aircraft_->CDfCL_nCL
1196 #define CDfCLI aircraft_->CDfCLI
1198 double CDfade_aArray[100][100];
1199 double CDfade_deArray[100];
1200 double CDfade_CDArray[100][100];
1201 int CDfade_nAlphaArray[100];
1204 #define CDfade aircraft_->CDfade
1205 #define CDfade_aArray aircraft_->CDfade_aArray
1206 #define CDfade_deArray aircraft_->CDfade_deArray
1207 #define CDfade_CDArray aircraft_->CDfade_CDArray
1208 #define CDfade_nAlphaArray aircraft_->CDfade_nAlphaArray
1209 #define CDfade_nde aircraft_->CDfade_nde
1210 #define CDfadeI aircraft_->CDfadeI
1212 double CDfdf_dfArray[100];
1213 double CDfdf_CDArray[100];
1216 #define CDfdf aircraft_->CDfdf
1217 #define CDfdf_dfArray aircraft_->CDfdf_dfArray
1218 #define CDfdf_CDArray aircraft_->CDfdf_CDArray
1219 #define CDfdf_ndf aircraft_->CDfdf_ndf
1220 #define CDfdfI aircraft_->CDfdfI
1222 double CDfadf_aArray[100][100];
1223 double CDfadf_dfArray[100];
1224 double CDfadf_CDArray[100][100];
1225 int CDfadf_nAlphaArray[100];
1228 #define CDfadf aircraft_->CDfadf
1229 #define CDfadf_aArray aircraft_->CDfadf_aArray
1230 #define CDfadf_dfArray aircraft_->CDfadf_dfArray
1231 #define CDfadf_CDArray aircraft_->CDfadf_CDArray
1232 #define CDfadf_nAlphaArray aircraft_->CDfadf_nAlphaArray
1233 #define CDfadf_ndf aircraft_->CDfadf_ndf
1234 #define CDfadfI aircraft_->CDfadfI
1235 double CXo, CXK, CX_a, CX_a2, CX_a3, CX_adot;
1236 double CX_q, CX_de, CX_dr, CX_df, CX_adf;
1237 #define CXo aircraft_->CXo
1238 #define CXK aircraft_->CXK
1239 #define CX_a aircraft_->CX_a
1240 #define CX_a2 aircraft_->CX_a2
1241 #define CX_a3 aircraft_->CX_a3
1242 #define CX_adot aircraft_->CX_adot
1243 #define CX_q aircraft_->CX_q
1244 #define CX_de aircraft_->CX_de
1245 #define CX_dr aircraft_->CX_dr
1246 #define CX_df aircraft_->CX_df
1247 #define CX_adf aircraft_->CX_adf
1248 double CXfabetaf_aArray[30][100][100];
1249 double CXfabetaf_betaArray[30][100];
1250 double CXfabetaf_CXArray[30][100][100];
1251 int CXfabetaf_nAlphaArray[30][100];
1252 int CXfabetaf_nbeta[30];
1253 double CXfabetaf_fArray[30];
1256 int CXfabetaf_nice, CXfabetaf_na_nice, CXfabetaf_nb_nice;
1257 double CXfabetaf_bArray_nice[100];
1258 double CXfabetaf_aArray_nice[100];
1259 #define CXfabetaf_aArray aircraft_->CXfabetaf_aArray
1260 #define CXfabetaf_betaArray aircraft_->CXfabetaf_betaArray
1261 #define CXfabetaf_CXArray aircraft_->CXfabetaf_CXArray
1262 #define CXfabetaf_nAlphaArray aircraft_->CXfabetaf_nAlphaArray
1263 #define CXfabetaf_nbeta aircraft_->CXfabetaf_nbeta
1264 #define CXfabetaf_fArray aircraft_->CXfabetaf_fArray
1265 #define CXfabetaf_nf aircraft_->CXfabetaf_nf
1266 #define CXfabetafI aircraft_->CXfabetafI
1267 #define CXfabetaf_nice aircraft_->CXfabetaf_nice
1268 #define CXfabetaf_na_nice aircraft_->CXfabetaf_na_nice
1269 #define CXfabetaf_nb_nice aircraft_->CXfabetaf_nb_nice
1270 #define CXfabetaf_bArray_nice aircraft_->CXfabetaf_bArray_nice
1271 #define CXfabetaf_aArray_nice aircraft_->CXfabetaf_aArray_nice
1272 double CXfadef_aArray[30][100][100];
1273 double CXfadef_deArray[30][100];
1274 double CXfadef_CXArray[30][100][100];
1275 int CXfadef_nAlphaArray[30][100];
1276 int CXfadef_nde[30];
1277 double CXfadef_fArray[30];
1280 int CXfadef_nice, CXfadef_na_nice, CXfadef_nde_nice;
1281 double CXfadef_deArray_nice[100];
1282 double CXfadef_aArray_nice[100];
1283 #define CXfadef_aArray aircraft_->CXfadef_aArray
1284 #define CXfadef_deArray aircraft_->CXfadef_deArray
1285 #define CXfadef_CXArray aircraft_->CXfadef_CXArray
1286 #define CXfadef_nAlphaArray aircraft_->CXfadef_nAlphaArray
1287 #define CXfadef_nde aircraft_->CXfadef_nde
1288 #define CXfadef_fArray aircraft_->CXfadef_fArray
1289 #define CXfadef_nf aircraft_->CXfadef_nf
1290 #define CXfadefI aircraft_->CXfadefI
1291 #define CXfadef_nice aircraft_->CXfadef_nice
1292 #define CXfadef_na_nice aircraft_->CXfadef_na_nice
1293 #define CXfadef_nde_nice aircraft_->CXfadef_nde_nice
1294 #define CXfadef_deArray_nice aircraft_->CXfadef_deArray_nice
1295 #define CXfadef_aArray_nice aircraft_->CXfadef_aArray_nice
1296 double CXfaqf_aArray[30][100][100];
1297 double CXfaqf_qArray[30][100];
1298 double CXfaqf_CXArray[30][100][100];
1299 int CXfaqf_nAlphaArray[30][100];
1301 double CXfaqf_fArray[30];
1304 int CXfaqf_nice, CXfaqf_na_nice, CXfaqf_nq_nice;
1305 double CXfaqf_qArray_nice[100];
1306 double CXfaqf_aArray_nice[100];
1307 #define CXfaqf_aArray aircraft_->CXfaqf_aArray
1308 #define CXfaqf_qArray aircraft_->CXfaqf_qArray
1309 #define CXfaqf_CXArray aircraft_->CXfaqf_CXArray
1310 #define CXfaqf_nAlphaArray aircraft_->CXfaqf_nAlphaArray
1311 #define CXfaqf_nq aircraft_->CXfaqf_nq
1312 #define CXfaqf_fArray aircraft_->CXfaqf_fArray
1313 #define CXfaqf_nf aircraft_->CXfaqf_nf
1314 #define CXfaqfI aircraft_->CXfaqfI
1315 #define CXfaqf_nice aircraft_->CXfaqf_nice
1316 #define CXfaqf_na_nice aircraft_->CXfaqf_na_nice
1317 #define CXfaqf_nq_nice aircraft_->CXfaqf_nq_nice
1318 #define CXfaqf_qArray_nice aircraft_->CXfaqf_qArray_nice
1319 #define CXfaqf_aArray_nice aircraft_->CXfaqf_aArray_nice
1320 double CDo_save, CDK_save, CLK_save, CD_a_save, CD_adot_save, CD_q_save, CD_ih_save;
1321 double CD_de_save, CD_dr_save, CD_da_save, CD_beta_save;
1322 double CD_df_save, CD_ds_save, CD_dg_save;
1323 double CXo_save, CXK_save, CX_a_save, CX_a2_save, CX_a3_save;
1324 double CX_adot_save, CX_q_save, CX_de_save;
1325 double CX_dr_save, CX_df_save, CX_adf_save;
1326 #define CDo_save aircraft_->CDo_save
1327 #define CDK_save aircraft_->CDK_save
1328 #define CLK_save aircraft_->CLK_save
1329 #define CD_a_save aircraft_->CD_a_save
1330 #define CD_adot_save aircraft_->CD_adot_save
1331 #define CD_q_save aircraft_->CD_q_save
1332 #define CD_ih_save aircraft_->CD_ih_save
1333 #define CD_de_save aircraft_->CD_de_save
1334 #define CD_dr_save aircraft_->CD_dr_save
1335 #define CD_da_save aircraft_->CD_da_save
1336 #define CD_beta_save aircraft_->CD_beta_save
1337 #define CD_df_save aircraft_->CD_df_save
1338 #define CD_ds_save aircraft_->CD_ds_save
1339 #define CD_dg_save aircraft_->CD_dg_save
1340 #define CXo_save aircraft_->CXo_save
1341 #define CXK_save aircraft_->CXK_save
1342 #define CX_a_save aircraft_->CX_a_save
1343 #define CX_a2_save aircraft_->CX_a2_save
1344 #define CX_a3_save aircraft_->CX_a3_save
1345 #define CX_adot_save aircraft_->CX_adot_save
1346 #define CX_q_save aircraft_->CX_q_save
1347 #define CX_de_save aircraft_->CX_de_save
1348 #define CX_dr_save aircraft_->CX_dr_save
1349 #define CX_df_save aircraft_->CX_df_save
1350 #define CX_adf_save aircraft_->CX_adf_save
1353 /* Variables (token2) ===========================================*/
1354 /* CL ============ Aerodynamic z-force quantities (longitudinal) */
1356 std::map <string,int> CL_map;
1357 #define CL_map aircraft_->CL_map
1359 double CLo, CL_a, CL_adot, CL_q, CL_ih, CL_de;
1360 double CL_df, CL_ds, CL_dg;
1361 #define CLo aircraft_->CLo
1362 #define CL_a aircraft_->CL_a
1363 #define CL_adot aircraft_->CL_adot
1364 #define CL_q aircraft_->CL_q
1365 #define CL_ih aircraft_->CL_ih
1366 #define CL_de aircraft_->CL_de
1367 #define CL_df aircraft_->CL_df
1368 #define CL_ds aircraft_->CL_ds
1369 #define CL_dg aircraft_->CL_dg
1371 double CLfa_aArray[100];
1372 double CLfa_CLArray[100];
1375 #define CLfa aircraft_->CLfa
1376 #define CLfa_aArray aircraft_->CLfa_aArray
1377 #define CLfa_CLArray aircraft_->CLfa_CLArray
1378 #define CLfa_nAlpha aircraft_->CLfa_nAlpha
1379 #define CLfaI aircraft_->CLfaI
1381 double CLfade_aArray[100][100];
1382 double CLfade_deArray[100];
1383 double CLfade_CLArray[100][100];
1384 int CLfade_nAlphaArray[100];
1387 #define CLfade aircraft_->CLfade
1388 #define CLfade_aArray aircraft_->CLfade_aArray
1389 #define CLfade_deArray aircraft_->CLfade_deArray
1390 #define CLfade_CLArray aircraft_->CLfade_CLArray
1391 #define CLfade_nAlphaArray aircraft_->CLfade_nAlphaArray
1392 #define CLfade_nde aircraft_->CLfade_nde
1393 #define CLfadeI aircraft_->CLfadeI
1395 double CLfdf_dfArray[100];
1396 double CLfdf_CLArray[100];
1399 #define CLfdf aircraft_->CLfdf
1400 #define CLfdf_dfArray aircraft_->CLfdf_dfArray
1401 #define CLfdf_CLArray aircraft_->CLfdf_CLArray
1402 #define CLfdf_ndf aircraft_->CLfdf_ndf
1403 #define CLfdfI aircraft_->CLfdfI
1405 double CLfadf_aArray[100][100];
1406 double CLfadf_dfArray[100];
1407 double CLfadf_CLArray[100][100];
1408 int CLfadf_nAlphaArray[100];
1411 #define CLfadf aircraft_->CLfadf
1412 #define CLfadf_aArray aircraft_->CLfadf_aArray
1413 #define CLfadf_dfArray aircraft_->CLfadf_dfArray
1414 #define CLfadf_CLArray aircraft_->CLfadf_CLArray
1415 #define CLfadf_nAlphaArray aircraft_->CLfadf_nAlphaArray
1416 #define CLfadf_ndf aircraft_->CLfadf_ndf
1417 #define CLfadfI aircraft_->CLfadfI
1418 double CZo, CZ_a, CZ_a2, CZ_a3, CZ_adot;
1419 double CZ_q, CZ_de, CZ_deb2, CZ_df, CZ_adf;
1420 #define CZo aircraft_->CZo
1421 #define CZ_a aircraft_->CZ_a
1422 #define CZ_a2 aircraft_->CZ_a2
1423 #define CZ_a3 aircraft_->CZ_a3
1424 #define CZ_adot aircraft_->CZ_adot
1425 #define CZ_q aircraft_->CZ_q
1426 #define CZ_de aircraft_->CZ_de
1427 #define CZ_deb2 aircraft_->CZ_deb2
1428 #define CZ_df aircraft_->CZ_df
1429 #define CZ_adf aircraft_->CZ_adf
1431 double CZfa_aArray[100];
1432 double CZfa_CZArray[100];
1435 #define CZfa aircraft_->CZfa
1436 #define CZfa_aArray aircraft_->CZfa_aArray
1437 #define CZfa_CZArray aircraft_->CZfa_CZArray
1438 #define CZfa_nAlpha aircraft_->CZfa_nAlpha
1439 #define CZfaI aircraft_->CZfaI
1440 double CZfabetaf_aArray[30][100][100];
1441 double CZfabetaf_betaArray[30][100];
1442 double CZfabetaf_CZArray[30][100][100];
1443 int CZfabetaf_nAlphaArray[30][100];
1444 int CZfabetaf_nbeta[30];
1445 double CZfabetaf_fArray[30];
1448 int CZfabetaf_nice, CZfabetaf_na_nice, CZfabetaf_nb_nice;
1449 double CZfabetaf_bArray_nice[100];
1450 double CZfabetaf_aArray_nice[100];
1451 #define CZfabetaf_aArray aircraft_->CZfabetaf_aArray
1452 #define CZfabetaf_betaArray aircraft_->CZfabetaf_betaArray
1453 #define CZfabetaf_CZArray aircraft_->CZfabetaf_CZArray
1454 #define CZfabetaf_nAlphaArray aircraft_->CZfabetaf_nAlphaArray
1455 #define CZfabetaf_nbeta aircraft_->CZfabetaf_nbeta
1456 #define CZfabetaf_fArray aircraft_->CZfabetaf_fArray
1457 #define CZfabetaf_nf aircraft_->CZfabetaf_nf
1458 #define CZfabetafI aircraft_->CZfabetafI
1459 #define CZfabetaf_nice aircraft_->CZfabetaf_nice
1460 #define CZfabetaf_na_nice aircraft_->CZfabetaf_na_nice
1461 #define CZfabetaf_nb_nice aircraft_->CZfabetaf_nb_nice
1462 #define CZfabetaf_bArray_nice aircraft_->CZfabetaf_bArray_nice
1463 #define CZfabetaf_aArray_nice aircraft_->CZfabetaf_aArray_nice
1464 double CZfadef_aArray[30][100][100];
1465 double CZfadef_deArray[30][100];
1466 double CZfadef_CZArray[30][100][100];
1467 int CZfadef_nAlphaArray[30][100];
1468 int CZfadef_nde[30];
1469 double CZfadef_fArray[30];
1472 int CZfadef_nice, CZfadef_na_nice, CZfadef_nde_nice;
1473 double CZfadef_deArray_nice[100];
1474 double CZfadef_aArray_nice[100];
1475 #define CZfadef_aArray aircraft_->CZfadef_aArray
1476 #define CZfadef_deArray aircraft_->CZfadef_deArray
1477 #define CZfadef_CZArray aircraft_->CZfadef_CZArray
1478 #define CZfadef_nAlphaArray aircraft_->CZfadef_nAlphaArray
1479 #define CZfadef_nde aircraft_->CZfadef_nde
1480 #define CZfadef_fArray aircraft_->CZfadef_fArray
1481 #define CZfadef_nf aircraft_->CZfadef_nf
1482 #define CZfadefI aircraft_->CZfadefI
1483 #define CZfadef_nice aircraft_->CZfadef_nice
1484 #define CZfadef_na_nice aircraft_->CZfadef_na_nice
1485 #define CZfadef_nde_nice aircraft_->CZfadef_nde_nice
1486 #define CZfadef_deArray_nice aircraft_->CZfadef_deArray_nice
1487 #define CZfadef_aArray_nice aircraft_->CZfadef_aArray_nice
1488 double CZfaqf_aArray[30][100][100];
1489 double CZfaqf_qArray[30][100];
1490 double CZfaqf_CZArray[30][100][100];
1491 int CZfaqf_nAlphaArray[30][100];
1493 double CZfaqf_fArray[30];
1496 int CZfaqf_nice, CZfaqf_na_nice, CZfaqf_nq_nice;
1497 double CZfaqf_qArray_nice[100];
1498 double CZfaqf_aArray_nice[100];
1499 #define CZfaqf_aArray aircraft_->CZfaqf_aArray
1500 #define CZfaqf_qArray aircraft_->CZfaqf_qArray
1501 #define CZfaqf_CZArray aircraft_->CZfaqf_CZArray
1502 #define CZfaqf_nAlphaArray aircraft_->CZfaqf_nAlphaArray
1503 #define CZfaqf_nq aircraft_->CZfaqf_nq
1504 #define CZfaqf_fArray aircraft_->CZfaqf_fArray
1505 #define CZfaqf_nf aircraft_->CZfaqf_nf
1506 #define CZfaqfI aircraft_->CZfaqfI
1507 #define CZfaqf_nice aircraft_->CZfaqf_nice
1508 #define CZfaqf_na_nice aircraft_->CZfaqf_na_nice
1509 #define CZfaqf_nq_nice aircraft_->CZfaqf_nq_nice
1510 #define CZfaqf_qArray_nice aircraft_->CZfaqf_qArray_nice
1511 #define CZfaqf_aArray_nice aircraft_->CZfaqf_aArray_nice
1512 double CLo_save, CL_a_save, CL_adot_save;
1513 double CL_q_save, CL_ih_save, CL_de_save;
1514 double CL_df_save, CL_ds_save, CL_dg_save;
1515 double CZo_save, CZ_a_save, CZ_a2_save;
1516 double CZ_a3_save, CZ_adot_save, CZ_q_save;
1517 double CZ_de_save, CZ_deb2_save, CZ_df_save;
1519 #define CLo_save aircraft_->CLo_save
1520 #define CL_a_save aircraft_->CL_a_save
1521 #define CL_adot_save aircraft_->CL_adot_save
1522 #define CL_q_save aircraft_->CL_q_save
1523 #define CL_ih_save aircraft_->CL_ih_save
1524 #define CL_de_save aircraft_->CL_de_save
1525 #define CL_df_save aircraft_->CL_df_save
1526 #define CL_ds_save aircraft_->CL_ds_save
1527 #define CL_dg_save aircraft_->CL_dg_save
1528 #define CZo_save aircraft_->CZo_save
1529 #define CZ_a_save aircraft_->CZ_a_save
1530 #define CZ_a2_save aircraft_->CZ_a2_save
1531 #define CZ_a3_save aircraft_->CZ_a3_save
1532 #define CZ_adot_save aircraft_->CZ_adot_save
1533 #define CZ_q_save aircraft_->CZ_q_save
1534 #define CZ_de_save aircraft_->CZ_de_save
1535 #define CZ_deb2_save aircraft_->CZ_deb2_save
1536 #define CZ_df_save aircraft_->CZ_df_save
1537 #define CZ_adf_save aircraft_->CZ_adf_save
1540 /* Variables (token2) ===========================================*/
1541 /* Cm ============ Aerodynamic m-moment quantities (longitudinal) */
1543 std::map <string,int> Cm_map;
1544 #define Cm_map aircraft_->Cm_map
1546 double Cmo, Cm_a, Cm_a2, Cm_adot, Cm_q;
1547 double Cm_ih, Cm_de, Cm_b2, Cm_r;
1548 double Cm_df, Cm_ds, Cm_dg;
1549 #define Cmo aircraft_->Cmo
1550 #define Cm_a aircraft_->Cm_a
1551 #define Cm_a2 aircraft_->Cm_a2
1552 #define Cm_adot aircraft_->Cm_adot
1553 #define Cm_q aircraft_->Cm_q
1554 #define Cm_ih aircraft_->Cm_ih
1555 #define Cm_de aircraft_->Cm_de
1556 #define Cm_b2 aircraft_->Cm_b2
1557 #define Cm_r aircraft_->Cm_r
1558 #define Cm_df aircraft_->Cm_df
1559 #define Cm_ds aircraft_->Cm_ds
1560 #define Cm_dg aircraft_->Cm_dg
1562 double Cmfa_aArray[100];
1563 double Cmfa_CmArray[100];
1566 #define Cmfa aircraft_->Cmfa
1567 #define Cmfa_aArray aircraft_->Cmfa_aArray
1568 #define Cmfa_CmArray aircraft_->Cmfa_CmArray
1569 #define Cmfa_nAlpha aircraft_->Cmfa_nAlpha
1570 #define CmfaI aircraft_->CmfaI
1572 double Cmfade_aArray[100][100];
1573 double Cmfade_deArray[100];
1574 double Cmfade_CmArray[100][100];
1575 int Cmfade_nAlphaArray[100];
1578 #define Cmfade aircraft_->Cmfade
1579 #define Cmfade_aArray aircraft_->Cmfade_aArray
1580 #define Cmfade_deArray aircraft_->Cmfade_deArray
1581 #define Cmfade_CmArray aircraft_->Cmfade_CmArray
1582 #define Cmfade_nAlphaArray aircraft_->Cmfade_nAlphaArray
1583 #define Cmfade_nde aircraft_->Cmfade_nde
1584 #define CmfadeI aircraft_->CmfadeI
1586 // induced flow in slipstream impinging on tail
1588 #define w_induced aircraft_->w_induced
1592 double Cmfdf_dfArray[100];
1593 double Cmfdf_CmArray[100];
1596 #define Cmfdf aircraft_->Cmfdf
1597 #define Cmfdf_dfArray aircraft_->Cmfdf_dfArray
1598 #define Cmfdf_CmArray aircraft_->Cmfdf_CmArray
1599 #define Cmfdf_ndf aircraft_->Cmfdf_ndf
1600 #define CmfdfI aircraft_->CmfdfI
1602 double Cmfadf_aArray[100][100];
1603 double Cmfadf_dfArray[100];
1604 double Cmfadf_CmArray[100][100];
1605 int Cmfadf_nAlphaArray[100];
1608 #define Cmfadf aircraft_->Cmfadf
1609 #define Cmfadf_aArray aircraft_->Cmfadf_aArray
1610 #define Cmfadf_dfArray aircraft_->Cmfadf_dfArray
1611 #define Cmfadf_CmArray aircraft_->Cmfadf_CmArray
1612 #define Cmfadf_nAlphaArray aircraft_->Cmfadf_nAlphaArray
1613 #define Cmfadf_ndf aircraft_->Cmfadf_ndf
1614 #define CmfadfI aircraft_->CmfadfI
1615 double Cmfabetaf_aArray[30][100][100];
1616 double Cmfabetaf_betaArray[30][100];
1617 double Cmfabetaf_CmArray[30][100][100];
1618 int Cmfabetaf_nAlphaArray[30][100];
1619 int Cmfabetaf_nbeta[30];
1620 double Cmfabetaf_fArray[30];
1623 int Cmfabetaf_nice, Cmfabetaf_na_nice, Cmfabetaf_nb_nice;
1624 double Cmfabetaf_bArray_nice[100];
1625 double Cmfabetaf_aArray_nice[100];
1626 #define Cmfabetaf_aArray aircraft_->Cmfabetaf_aArray
1627 #define Cmfabetaf_betaArray aircraft_->Cmfabetaf_betaArray
1628 #define Cmfabetaf_CmArray aircraft_->Cmfabetaf_CmArray
1629 #define Cmfabetaf_nAlphaArray aircraft_->Cmfabetaf_nAlphaArray
1630 #define Cmfabetaf_nbeta aircraft_->Cmfabetaf_nbeta
1631 #define Cmfabetaf_fArray aircraft_->Cmfabetaf_fArray
1632 #define Cmfabetaf_nf aircraft_->Cmfabetaf_nf
1633 #define CmfabetafI aircraft_->CmfabetafI
1634 #define Cmfabetaf_nice aircraft_->Cmfabetaf_nice
1635 #define Cmfabetaf_na_nice aircraft_->Cmfabetaf_na_nice
1636 #define Cmfabetaf_nb_nice aircraft_->Cmfabetaf_nb_nice
1637 #define Cmfabetaf_bArray_nice aircraft_->Cmfabetaf_bArray_nice
1638 #define Cmfabetaf_aArray_nice aircraft_->Cmfabetaf_aArray_nice
1639 double Cmfadef_aArray[30][100][100];
1640 double Cmfadef_deArray[30][100];
1641 double Cmfadef_CmArray[30][100][100];
1642 int Cmfadef_nAlphaArray[30][100];
1643 int Cmfadef_nde[30];
1644 double Cmfadef_fArray[30];
1647 int Cmfadef_nice, Cmfadef_na_nice, Cmfadef_nde_nice;
1648 double Cmfadef_deArray_nice[100];
1649 double Cmfadef_aArray_nice[100];
1650 #define Cmfadef_aArray aircraft_->Cmfadef_aArray
1651 #define Cmfadef_deArray aircraft_->Cmfadef_deArray
1652 #define Cmfadef_CmArray aircraft_->Cmfadef_CmArray
1653 #define Cmfadef_nAlphaArray aircraft_->Cmfadef_nAlphaArray
1654 #define Cmfadef_nde aircraft_->Cmfadef_nde
1655 #define Cmfadef_fArray aircraft_->Cmfadef_fArray
1656 #define Cmfadef_nf aircraft_->Cmfadef_nf
1657 #define CmfadefI aircraft_->CmfadefI
1658 #define Cmfadef_nice aircraft_->Cmfadef_nice
1659 #define Cmfadef_na_nice aircraft_->Cmfadef_na_nice
1660 #define Cmfadef_nde_nice aircraft_->Cmfadef_nde_nice
1661 #define Cmfadef_deArray_nice aircraft_->Cmfadef_deArray_nice
1662 #define Cmfadef_aArray_nice aircraft_->Cmfadef_aArray_nice
1663 double Cmfaqf_aArray[30][100][100];
1664 double Cmfaqf_qArray[30][100];
1665 double Cmfaqf_CmArray[30][100][100];
1666 int Cmfaqf_nAlphaArray[30][100];
1668 double Cmfaqf_fArray[30];
1671 int Cmfaqf_nice, Cmfaqf_na_nice, Cmfaqf_nq_nice;
1672 double Cmfaqf_qArray_nice[100];
1673 double Cmfaqf_aArray_nice[100];
1674 #define Cmfaqf_aArray aircraft_->Cmfaqf_aArray
1675 #define Cmfaqf_qArray aircraft_->Cmfaqf_qArray
1676 #define Cmfaqf_CmArray aircraft_->Cmfaqf_CmArray
1677 #define Cmfaqf_nAlphaArray aircraft_->Cmfaqf_nAlphaArray
1678 #define Cmfaqf_nq aircraft_->Cmfaqf_nq
1679 #define Cmfaqf_fArray aircraft_->Cmfaqf_fArray
1680 #define Cmfaqf_nf aircraft_->Cmfaqf_nf
1681 #define CmfaqfI aircraft_->CmfaqfI
1682 #define Cmfaqf_nice aircraft_->Cmfaqf_nice
1683 #define Cmfaqf_na_nice aircraft_->Cmfaqf_na_nice
1684 #define Cmfaqf_nq_nice aircraft_->Cmfaqf_nq_nice
1685 #define Cmfaqf_qArray_nice aircraft_->Cmfaqf_qArray_nice
1686 #define Cmfaqf_aArray_nice aircraft_->Cmfaqf_aArray_nice
1687 double Cmo_save, Cm_a_save, Cm_a2_save, Cm_adot_save, Cm_q_save, Cm_ih_save;
1688 double Cm_de_save, Cm_b2_save, Cm_r_save;
1689 double Cm_df_save, Cm_ds_save, Cm_dg_save;
1690 #define Cmo_save aircraft_->Cmo_save
1691 #define Cm_a_save aircraft_->Cm_a_save
1692 #define Cm_a2_save aircraft_->Cm_a2_save
1693 #define Cm_adot_save aircraft_->Cm_adot_save
1694 #define Cm_q_save aircraft_->Cm_q_save
1695 #define Cm_ih_save aircraft_->Cm_ih_save
1696 #define Cm_de_save aircraft_->Cm_de_save
1697 #define Cm_b2_save aircraft_->Cm_b2_save
1698 #define Cm_r_save aircraft_->Cm_r_save
1699 #define Cm_df_save aircraft_->Cm_df_save
1700 #define Cm_ds_save aircraft_->Cm_ds_save
1701 #define Cm_dg_save aircraft_->Cm_dg_save
1704 /* Variables (token2) ===========================================*/
1705 /* CY ============ Aerodynamic y-force quantities (lateral) =====*/
1707 std::map <string,int> CY_map;
1708 #define CY_map aircraft_->CY_map
1710 double CYo, CY_beta, CY_p, CY_r, CY_da, CY_dr, CY_dra, CY_bdot;
1711 #define CYo aircraft_->CYo
1712 #define CY_beta aircraft_->CY_beta
1713 #define CY_p aircraft_->CY_p
1714 #define CY_r aircraft_->CY_r
1715 #define CY_da aircraft_->CY_da
1716 #define CY_dr aircraft_->CY_dr
1717 #define CY_dra aircraft_->CY_dra
1718 #define CY_bdot aircraft_->CY_bdot
1720 double CYfada_aArray[100][100];
1721 double CYfada_daArray[100];
1722 double CYfada_CYArray[100][100];
1723 int CYfada_nAlphaArray[100];
1726 #define CYfada aircraft_->CYfada
1727 #define CYfada_aArray aircraft_->CYfada_aArray
1728 #define CYfada_daArray aircraft_->CYfada_daArray
1729 #define CYfada_CYArray aircraft_->CYfada_CYArray
1730 #define CYfada_nAlphaArray aircraft_->CYfada_nAlphaArray
1731 #define CYfada_nda aircraft_->CYfada_nda
1732 #define CYfadaI aircraft_->CYfadaI
1734 double CYfbetadr_betaArray[100][100];
1735 double CYfbetadr_drArray[100];
1736 double CYfbetadr_CYArray[100][100];
1737 int CYfbetadr_nBetaArray[100];
1740 #define CYfbetadr aircraft_->CYfbetadr
1741 #define CYfbetadr_betaArray aircraft_->CYfbetadr_betaArray
1742 #define CYfbetadr_drArray aircraft_->CYfbetadr_drArray
1743 #define CYfbetadr_CYArray aircraft_->CYfbetadr_CYArray
1744 #define CYfbetadr_nBetaArray aircraft_->CYfbetadr_nBetaArray
1745 #define CYfbetadr_ndr aircraft_->CYfbetadr_ndr
1746 #define CYfbetadrI aircraft_->CYfbetadrI
1747 double CYfabetaf_aArray[30][100][100];
1748 double CYfabetaf_betaArray[30][100];
1749 double CYfabetaf_CYArray[30][100][100];
1750 int CYfabetaf_nAlphaArray[30][100];
1751 int CYfabetaf_nbeta[30];
1752 double CYfabetaf_fArray[30];
1755 int CYfabetaf_nice, CYfabetaf_na_nice, CYfabetaf_nb_nice;
1756 double CYfabetaf_bArray_nice[100];
1757 double CYfabetaf_aArray_nice[100];
1758 #define CYfabetaf_aArray aircraft_->CYfabetaf_aArray
1759 #define CYfabetaf_betaArray aircraft_->CYfabetaf_betaArray
1760 #define CYfabetaf_CYArray aircraft_->CYfabetaf_CYArray
1761 #define CYfabetaf_nAlphaArray aircraft_->CYfabetaf_nAlphaArray
1762 #define CYfabetaf_nbeta aircraft_->CYfabetaf_nbeta
1763 #define CYfabetaf_fArray aircraft_->CYfabetaf_fArray
1764 #define CYfabetaf_nf aircraft_->CYfabetaf_nf
1765 #define CYfabetafI aircraft_->CYfabetafI
1766 #define CYfabetaf_nice aircraft_->CYfabetaf_nice
1767 #define CYfabetaf_na_nice aircraft_->CYfabetaf_na_nice
1768 #define CYfabetaf_nb_nice aircraft_->CYfabetaf_nb_nice
1769 #define CYfabetaf_bArray_nice aircraft_->CYfabetaf_bArray_nice
1770 #define CYfabetaf_aArray_nice aircraft_->CYfabetaf_aArray_nice
1771 double CYfadaf_aArray[30][100][100];
1772 double CYfadaf_daArray[30][100];
1773 double CYfadaf_CYArray[30][100][100];
1774 int CYfadaf_nAlphaArray[30][100];
1775 int CYfadaf_nda[30];
1776 double CYfadaf_fArray[30];
1779 int CYfadaf_nice, CYfadaf_na_nice, CYfadaf_nda_nice;
1780 double CYfadaf_daArray_nice[100];
1781 double CYfadaf_aArray_nice[100];
1782 #define CYfadaf_aArray aircraft_->CYfadaf_aArray
1783 #define CYfadaf_daArray aircraft_->CYfadaf_daArray
1784 #define CYfadaf_CYArray aircraft_->CYfadaf_CYArray
1785 #define CYfadaf_nAlphaArray aircraft_->CYfadaf_nAlphaArray
1786 #define CYfadaf_nda aircraft_->CYfadaf_nda
1787 #define CYfadaf_fArray aircraft_->CYfadaf_fArray
1788 #define CYfadaf_nf aircraft_->CYfadaf_nf
1789 #define CYfadafI aircraft_->CYfadafI
1790 #define CYfadaf_nice aircraft_->CYfadaf_nice
1791 #define CYfadaf_na_nice aircraft_->CYfadaf_na_nice
1792 #define CYfadaf_nda_nice aircraft_->CYfadaf_nda_nice
1793 #define CYfadaf_daArray_nice aircraft_->CYfadaf_daArray_nice
1794 #define CYfadaf_aArray_nice aircraft_->CYfadaf_aArray_nice
1795 double CYfadrf_aArray[30][100][100];
1796 double CYfadrf_drArray[30][100];
1797 double CYfadrf_CYArray[30][100][100];
1798 int CYfadrf_nAlphaArray[30][100];
1799 int CYfadrf_ndr[30];
1800 double CYfadrf_fArray[30];
1803 int CYfadrf_nice, CYfadrf_na_nice, CYfadrf_ndr_nice;
1804 double CYfadrf_drArray_nice[100];
1805 double CYfadrf_aArray_nice[100];
1806 #define CYfadrf_aArray aircraft_->CYfadrf_aArray
1807 #define CYfadrf_drArray aircraft_->CYfadrf_drArray
1808 #define CYfadrf_CYArray aircraft_->CYfadrf_CYArray
1809 #define CYfadrf_nAlphaArray aircraft_->CYfadrf_nAlphaArray
1810 #define CYfadrf_ndr aircraft_->CYfadrf_ndr
1811 #define CYfadrf_fArray aircraft_->CYfadrf_fArray
1812 #define CYfadrf_nf aircraft_->CYfadrf_nf
1813 #define CYfadrfI aircraft_->CYfadrfI
1814 #define CYfadrf_nice aircraft_->CYfadrf_nice
1815 #define CYfadrf_na_nice aircraft_->CYfadrf_na_nice
1816 #define CYfadrf_ndr_nice aircraft_->CYfadrf_ndr_nice
1817 #define CYfadrf_drArray_nice aircraft_->CYfadrf_drArray_nice
1818 #define CYfadrf_aArray_nice aircraft_->CYfadrf_aArray_nice
1819 double CYfapf_aArray[30][100][100];
1820 double CYfapf_pArray[30][100];
1821 double CYfapf_CYArray[30][100][100];
1822 int CYfapf_nAlphaArray[30][100];
1824 double CYfapf_fArray[30];
1827 int CYfapf_nice, CYfapf_na_nice, CYfapf_np_nice;
1828 double CYfapf_pArray_nice[100];
1829 double CYfapf_aArray_nice[100];
1830 #define CYfapf_aArray aircraft_->CYfapf_aArray
1831 #define CYfapf_pArray aircraft_->CYfapf_pArray
1832 #define CYfapf_CYArray aircraft_->CYfapf_CYArray
1833 #define CYfapf_nAlphaArray aircraft_->CYfapf_nAlphaArray
1834 #define CYfapf_np aircraft_->CYfapf_np
1835 #define CYfapf_fArray aircraft_->CYfapf_fArray
1836 #define CYfapf_nf aircraft_->CYfapf_nf
1837 #define CYfapfI aircraft_->CYfapfI
1838 #define CYfapf_nice aircraft_->CYfapf_nice
1839 #define CYfapf_na_nice aircraft_->CYfapf_na_nice
1840 #define CYfapf_np_nice aircraft_->CYfapf_np_nice
1841 #define CYfapf_pArray_nice aircraft_->CYfapf_pArray_nice
1842 #define CYfapf_aArray_nice aircraft_->CYfapf_aArray_nice
1843 double CYfarf_aArray[30][100][100];
1844 double CYfarf_rArray[30][100];
1845 double CYfarf_CYArray[30][100][100];
1846 int CYfarf_nAlphaArray[30][100];
1848 double CYfarf_fArray[30];
1851 int CYfarf_nice, CYfarf_na_nice, CYfarf_nr_nice;
1852 double CYfarf_rArray_nice[100];
1853 double CYfarf_aArray_nice[100];
1854 #define CYfarf_aArray aircraft_->CYfarf_aArray
1855 #define CYfarf_rArray aircraft_->CYfarf_rArray
1856 #define CYfarf_CYArray aircraft_->CYfarf_CYArray
1857 #define CYfarf_nAlphaArray aircraft_->CYfarf_nAlphaArray
1858 #define CYfarf_nr aircraft_->CYfarf_nr
1859 #define CYfarf_fArray aircraft_->CYfarf_fArray
1860 #define CYfarf_nf aircraft_->CYfarf_nf
1861 #define CYfarfI aircraft_->CYfarfI
1862 #define CYfarf_nice aircraft_->CYfarf_nice
1863 #define CYfarf_na_nice aircraft_->CYfarf_na_nice
1864 #define CYfarf_nr_nice aircraft_->CYfarf_nr_nice
1865 #define CYfarf_rArray_nice aircraft_->CYfarf_rArray_nice
1866 #define CYfarf_aArray_nice aircraft_->CYfarf_aArray_nice
1867 double CYo_save, CY_beta_save, CY_p_save, CY_r_save, CY_da_save, CY_dr_save;
1868 double CY_dra_save, CY_bdot_save;
1869 #define CYo_save aircraft_->CYo_save
1870 #define CY_beta_save aircraft_->CY_beta_save
1871 #define CY_p_save aircraft_->CY_p_save
1872 #define CY_r_save aircraft_->CY_r_save
1873 #define CY_da_save aircraft_->CY_da_save
1874 #define CY_dr_save aircraft_->CY_dr_save
1875 #define CY_dra_save aircraft_->CY_dra_save
1876 #define CY_bdot_save aircraft_->CY_bdot_save
1879 /* Variables (token2) ===========================================*/
1880 /* Cl ============ Aerodynamic l-moment quantities (lateral) ====*/
1882 std::map <string,int> Cl_map;
1883 #define Cl_map aircraft_->Cl_map
1885 double Clo, Cl_beta, Cl_p, Cl_r, Cl_da, Cl_dr, Cl_daa;
1886 #define Clo aircraft_->Clo
1887 #define Cl_beta aircraft_->Cl_beta
1888 #define Cl_p aircraft_->Cl_p
1889 #define Cl_r aircraft_->Cl_r
1890 #define Cl_da aircraft_->Cl_da
1891 #define Cl_dr aircraft_->Cl_dr
1892 #define Cl_daa aircraft_->Cl_daa
1894 double Clfada_aArray[100][100];
1895 double Clfada_daArray[100];
1896 double Clfada_ClArray[100][100];
1897 int Clfada_nAlphaArray[100];
1900 #define Clfada aircraft_->Clfada
1901 #define Clfada_aArray aircraft_->Clfada_aArray
1902 #define Clfada_daArray aircraft_->Clfada_daArray
1903 #define Clfada_ClArray aircraft_->Clfada_ClArray
1904 #define Clfada_nAlphaArray aircraft_->Clfada_nAlphaArray
1905 #define Clfada_nda aircraft_->Clfada_nda
1906 #define ClfadaI aircraft_->ClfadaI
1908 double Clfbetadr_betaArray[100][100];
1909 double Clfbetadr_drArray[100];
1910 double Clfbetadr_ClArray[100][100];
1911 int Clfbetadr_nBetaArray[100];
1914 #define Clfbetadr aircraft_->Clfbetadr
1915 #define Clfbetadr_betaArray aircraft_->Clfbetadr_betaArray
1916 #define Clfbetadr_drArray aircraft_->Clfbetadr_drArray
1917 #define Clfbetadr_ClArray aircraft_->Clfbetadr_ClArray
1918 #define Clfbetadr_nBetaArray aircraft_->Clfbetadr_nBetaArray
1919 #define Clfbetadr_ndr aircraft_->Clfbetadr_ndr
1920 #define ClfbetadrI aircraft_->ClfbetadrI
1921 double Clfabetaf_aArray[30][100][100];
1922 double Clfabetaf_betaArray[30][100];
1923 double Clfabetaf_ClArray[30][100][100];
1924 int Clfabetaf_nAlphaArray[30][100];
1925 int Clfabetaf_nbeta[30];
1926 double Clfabetaf_fArray[30];
1929 int Clfabetaf_nice, Clfabetaf_na_nice, Clfabetaf_nb_nice;
1930 double Clfabetaf_bArray_nice[100];
1931 double Clfabetaf_aArray_nice[100];
1932 #define Clfabetaf_aArray aircraft_->Clfabetaf_aArray
1933 #define Clfabetaf_betaArray aircraft_->Clfabetaf_betaArray
1934 #define Clfabetaf_ClArray aircraft_->Clfabetaf_ClArray
1935 #define Clfabetaf_nAlphaArray aircraft_->Clfabetaf_nAlphaArray
1936 #define Clfabetaf_nbeta aircraft_->Clfabetaf_nbeta
1937 #define Clfabetaf_fArray aircraft_->Clfabetaf_fArray
1938 #define Clfabetaf_nf aircraft_->Clfabetaf_nf
1939 #define ClfabetafI aircraft_->ClfabetafI
1940 #define Clfabetaf_nice aircraft_->Clfabetaf_nice
1941 #define Clfabetaf_na_nice aircraft_->Clfabetaf_na_nice
1942 #define Clfabetaf_nb_nice aircraft_->Clfabetaf_nb_nice
1943 #define Clfabetaf_bArray_nice aircraft_->Clfabetaf_bArray_nice
1944 #define Clfabetaf_aArray_nice aircraft_->Clfabetaf_aArray_nice
1945 double Clfadaf_aArray[30][100][100];
1946 double Clfadaf_daArray[30][100];
1947 double Clfadaf_ClArray[30][100][100];
1948 int Clfadaf_nAlphaArray[30][100];
1949 int Clfadaf_nda[30];
1950 double Clfadaf_fArray[30];
1953 int Clfadaf_nice, Clfadaf_na_nice, Clfadaf_nda_nice;
1954 double Clfadaf_daArray_nice[100];
1955 double Clfadaf_aArray_nice[100];
1956 #define Clfadaf_aArray aircraft_->Clfadaf_aArray
1957 #define Clfadaf_daArray aircraft_->Clfadaf_daArray
1958 #define Clfadaf_ClArray aircraft_->Clfadaf_ClArray
1959 #define Clfadaf_nAlphaArray aircraft_->Clfadaf_nAlphaArray
1960 #define Clfadaf_nda aircraft_->Clfadaf_nda
1961 #define Clfadaf_fArray aircraft_->Clfadaf_fArray
1962 #define Clfadaf_nf aircraft_->Clfadaf_nf
1963 #define ClfadafI aircraft_->ClfadafI
1964 #define Clfadaf_nice aircraft_->Clfadaf_nice
1965 #define Clfadaf_na_nice aircraft_->Clfadaf_na_nice
1966 #define Clfadaf_nda_nice aircraft_->Clfadaf_nda_nice
1967 #define Clfadaf_daArray_nice aircraft_->Clfadaf_daArray_nice
1968 #define Clfadaf_aArray_nice aircraft_->Clfadaf_aArray_nice
1969 double Clfadrf_aArray[30][100][100];
1970 double Clfadrf_drArray[30][100];
1971 double Clfadrf_ClArray[30][100][100];
1972 int Clfadrf_nAlphaArray[30][100];
1973 int Clfadrf_ndr[30];
1974 double Clfadrf_fArray[30];
1977 int Clfadrf_nice, Clfadrf_na_nice, Clfadrf_ndr_nice;
1978 double Clfadrf_drArray_nice[100];
1979 double Clfadrf_aArray_nice[100];
1980 #define Clfadrf_aArray aircraft_->Clfadrf_aArray
1981 #define Clfadrf_drArray aircraft_->Clfadrf_drArray
1982 #define Clfadrf_ClArray aircraft_->Clfadrf_ClArray
1983 #define Clfadrf_nAlphaArray aircraft_->Clfadrf_nAlphaArray
1984 #define Clfadrf_ndr aircraft_->Clfadrf_ndr
1985 #define Clfadrf_fArray aircraft_->Clfadrf_fArray
1986 #define Clfadrf_nf aircraft_->Clfadrf_nf
1987 #define ClfadrfI aircraft_->ClfadrfI
1988 #define Clfadrf_nice aircraft_->Clfadrf_nice
1989 #define Clfadrf_na_nice aircraft_->Clfadrf_na_nice
1990 #define Clfadrf_ndr_nice aircraft_->Clfadrf_ndr_nice
1991 #define Clfadrf_drArray_nice aircraft_->Clfadrf_drArray_nice
1992 #define Clfadrf_aArray_nice aircraft_->Clfadrf_aArray_nice
1993 double Clfapf_aArray[30][100][100];
1994 double Clfapf_pArray[30][100];
1995 double Clfapf_ClArray[30][100][100];
1996 int Clfapf_nAlphaArray[30][100];
1998 double Clfapf_fArray[30];
2001 int Clfapf_nice, Clfapf_na_nice, Clfapf_np_nice;
2002 double Clfapf_pArray_nice[100];
2003 double Clfapf_aArray_nice[100];
2004 #define Clfapf_aArray aircraft_->Clfapf_aArray
2005 #define Clfapf_pArray aircraft_->Clfapf_pArray
2006 #define Clfapf_ClArray aircraft_->Clfapf_ClArray
2007 #define Clfapf_nAlphaArray aircraft_->Clfapf_nAlphaArray
2008 #define Clfapf_np aircraft_->Clfapf_np
2009 #define Clfapf_fArray aircraft_->Clfapf_fArray
2010 #define Clfapf_nf aircraft_->Clfapf_nf
2011 #define ClfapfI aircraft_->ClfapfI
2012 #define Clfapf_nice aircraft_->Clfapf_nice
2013 #define Clfapf_na_nice aircraft_->Clfapf_na_nice
2014 #define Clfapf_np_nice aircraft_->Clfapf_np_nice
2015 #define Clfapf_pArray_nice aircraft_->Clfapf_pArray_nice
2016 #define Clfapf_aArray_nice aircraft_->Clfapf_aArray_nice
2017 double Clfarf_aArray[30][100][100];
2018 double Clfarf_rArray[30][100];
2019 double Clfarf_ClArray[30][100][100];
2020 int Clfarf_nAlphaArray[30][100];
2022 double Clfarf_fArray[30];
2025 int Clfarf_nice, Clfarf_na_nice, Clfarf_nr_nice;
2026 double Clfarf_rArray_nice[100];
2027 double Clfarf_aArray_nice[100];
2028 #define Clfarf_aArray aircraft_->Clfarf_aArray
2029 #define Clfarf_rArray aircraft_->Clfarf_rArray
2030 #define Clfarf_ClArray aircraft_->Clfarf_ClArray
2031 #define Clfarf_nAlphaArray aircraft_->Clfarf_nAlphaArray
2032 #define Clfarf_nr aircraft_->Clfarf_nr
2033 #define Clfarf_fArray aircraft_->Clfarf_fArray
2034 #define Clfarf_nf aircraft_->Clfarf_nf
2035 #define ClfarfI aircraft_->ClfarfI
2036 #define Clfarf_nice aircraft_->Clfarf_nice
2037 #define Clfarf_na_nice aircraft_->Clfarf_na_nice
2038 #define Clfarf_nr_nice aircraft_->Clfarf_nr_nice
2039 #define Clfarf_rArray_nice aircraft_->Clfarf_rArray_nice
2040 #define Clfarf_aArray_nice aircraft_->Clfarf_aArray_nice
2041 double Clo_save, Cl_beta_save, Cl_p_save, Cl_r_save, Cl_da_save;
2042 double Cl_dr_save, Cl_daa_save;
2043 #define Clo_save aircraft_->Clo_save
2044 #define Cl_beta_save aircraft_->Cl_beta_save
2045 #define Cl_p_save aircraft_->Cl_p_save
2046 #define Cl_r_save aircraft_->Cl_r_save
2047 #define Cl_da_save aircraft_->Cl_da_save
2048 #define Cl_dr_save aircraft_->Cl_dr_save
2049 #define Cl_daa_save aircraft_->Cl_daa_save
2052 /* Variables (token2) ===========================================*/
2053 /* Cn ============ Aerodynamic n-moment quantities (lateral) ====*/
2055 std::map <string,int> Cn_map;
2056 #define Cn_map aircraft_->Cn_map
2058 double Cno, Cn_beta, Cn_p, Cn_r, Cn_da, Cn_dr, Cn_q, Cn_b3;
2059 #define Cno aircraft_->Cno
2060 #define Cn_beta aircraft_->Cn_beta
2061 #define Cn_p aircraft_->Cn_p
2062 #define Cn_r aircraft_->Cn_r
2063 #define Cn_da aircraft_->Cn_da
2064 #define Cn_dr aircraft_->Cn_dr
2065 #define Cn_q aircraft_->Cn_q
2066 #define Cn_b3 aircraft_->Cn_b3
2068 double Cnfada_aArray[100][100];
2069 double Cnfada_daArray[100];
2070 double Cnfada_CnArray[100][100];
2071 int Cnfada_nAlphaArray[100];
2074 #define Cnfada aircraft_->Cnfada
2075 #define Cnfada_aArray aircraft_->Cnfada_aArray
2076 #define Cnfada_daArray aircraft_->Cnfada_daArray
2077 #define Cnfada_CnArray aircraft_->Cnfada_CnArray
2078 #define Cnfada_nAlphaArray aircraft_->Cnfada_nAlphaArray
2079 #define Cnfada_nda aircraft_->Cnfada_nda
2080 #define CnfadaI aircraft_->CnfadaI
2082 double Cnfbetadr_betaArray[100][100];
2083 double Cnfbetadr_drArray[100];
2084 double Cnfbetadr_CnArray[100][100];
2085 int Cnfbetadr_nBetaArray[100];
2088 #define Cnfbetadr aircraft_->Cnfbetadr
2089 #define Cnfbetadr_betaArray aircraft_->Cnfbetadr_betaArray
2090 #define Cnfbetadr_drArray aircraft_->Cnfbetadr_drArray
2091 #define Cnfbetadr_CnArray aircraft_->Cnfbetadr_CnArray
2092 #define Cnfbetadr_nBetaArray aircraft_->Cnfbetadr_nBetaArray
2093 #define Cnfbetadr_ndr aircraft_->Cnfbetadr_ndr
2094 #define CnfbetadrI aircraft_->CnfbetadrI
2095 double Cnfabetaf_aArray[30][100][100];
2096 double Cnfabetaf_betaArray[30][100];
2097 double Cnfabetaf_CnArray[30][100][100];
2098 int Cnfabetaf_nAlphaArray[30][100];
2099 int Cnfabetaf_nbeta[30];
2100 double Cnfabetaf_fArray[30];
2103 int Cnfabetaf_nice, Cnfabetaf_na_nice, Cnfabetaf_nb_nice;
2104 double Cnfabetaf_bArray_nice[100];
2105 double Cnfabetaf_aArray_nice[100];
2106 #define Cnfabetaf_aArray aircraft_->Cnfabetaf_aArray
2107 #define Cnfabetaf_betaArray aircraft_->Cnfabetaf_betaArray
2108 #define Cnfabetaf_CnArray aircraft_->Cnfabetaf_CnArray
2109 #define Cnfabetaf_nAlphaArray aircraft_->Cnfabetaf_nAlphaArray
2110 #define Cnfabetaf_nbeta aircraft_->Cnfabetaf_nbeta
2111 #define Cnfabetaf_fArray aircraft_->Cnfabetaf_fArray
2112 #define Cnfabetaf_nf aircraft_->Cnfabetaf_nf
2113 #define CnfabetafI aircraft_->CnfabetafI
2114 #define Cnfabetaf_nice aircraft_->Cnfabetaf_nice
2115 #define Cnfabetaf_na_nice aircraft_->Cnfabetaf_na_nice
2116 #define Cnfabetaf_nb_nice aircraft_->Cnfabetaf_nb_nice
2117 #define Cnfabetaf_bArray_nice aircraft_->Cnfabetaf_bArray_nice
2118 #define Cnfabetaf_aArray_nice aircraft_->Cnfabetaf_aArray_nice
2119 double Cnfadaf_aArray[30][100][100];
2120 double Cnfadaf_daArray[30][100];
2121 double Cnfadaf_CnArray[30][100][100];
2122 int Cnfadaf_nAlphaArray[30][100];
2123 int Cnfadaf_nda[30];
2124 double Cnfadaf_fArray[30];
2127 int Cnfadaf_nice, Cnfadaf_na_nice, Cnfadaf_nda_nice;
2128 double Cnfadaf_daArray_nice[100];
2129 double Cnfadaf_aArray_nice[100];
2130 #define Cnfadaf_aArray aircraft_->Cnfadaf_aArray
2131 #define Cnfadaf_daArray aircraft_->Cnfadaf_daArray
2132 #define Cnfadaf_CnArray aircraft_->Cnfadaf_CnArray
2133 #define Cnfadaf_nAlphaArray aircraft_->Cnfadaf_nAlphaArray
2134 #define Cnfadaf_nda aircraft_->Cnfadaf_nda
2135 #define Cnfadaf_fArray aircraft_->Cnfadaf_fArray
2136 #define Cnfadaf_nf aircraft_->Cnfadaf_nf
2137 #define CnfadafI aircraft_->CnfadafI
2138 #define Cnfadaf_nice aircraft_->Cnfadaf_nice
2139 #define Cnfadaf_na_nice aircraft_->Cnfadaf_na_nice
2140 #define Cnfadaf_nda_nice aircraft_->Cnfadaf_nda_nice
2141 #define Cnfadaf_daArray_nice aircraft_->Cnfadaf_daArray_nice
2142 #define Cnfadaf_aArray_nice aircraft_->Cnfadaf_aArray_nice
2143 double Cnfadrf_aArray[30][100][100];
2144 double Cnfadrf_drArray[30][100];
2145 double Cnfadrf_CnArray[30][100][100];
2146 int Cnfadrf_nAlphaArray[30][100];
2147 int Cnfadrf_ndr[30];
2148 double Cnfadrf_fArray[30];
2151 int Cnfadrf_nice, Cnfadrf_na_nice, Cnfadrf_ndr_nice;
2152 double Cnfadrf_drArray_nice[100];
2153 double Cnfadrf_aArray_nice[100];
2154 #define Cnfadrf_aArray aircraft_->Cnfadrf_aArray
2155 #define Cnfadrf_drArray aircraft_->Cnfadrf_drArray
2156 #define Cnfadrf_CnArray aircraft_->Cnfadrf_CnArray
2157 #define Cnfadrf_nAlphaArray aircraft_->Cnfadrf_nAlphaArray
2158 #define Cnfadrf_ndr aircraft_->Cnfadrf_ndr
2159 #define Cnfadrf_fArray aircraft_->Cnfadrf_fArray
2160 #define Cnfadrf_nf aircraft_->Cnfadrf_nf
2161 #define CnfadrfI aircraft_->CnfadrfI
2162 #define Cnfadrf_nice aircraft_->Cnfadrf_nice
2163 #define Cnfadrf_na_nice aircraft_->Cnfadrf_na_nice
2164 #define Cnfadrf_ndr_nice aircraft_->Cnfadrf_ndr_nice
2165 #define Cnfadrf_drArray_nice aircraft_->Cnfadrf_drArray_nice
2166 #define Cnfadrf_aArray_nice aircraft_->Cnfadrf_aArray_nice
2167 double Cnfapf_aArray[30][100][100];
2168 double Cnfapf_pArray[30][100];
2169 double Cnfapf_CnArray[30][100][100];
2170 int Cnfapf_nAlphaArray[30][100];
2172 double Cnfapf_fArray[30];
2175 int Cnfapf_nice, Cnfapf_na_nice, Cnfapf_np_nice;
2176 double Cnfapf_pArray_nice[100];
2177 double Cnfapf_aArray_nice[100];
2178 #define Cnfapf_aArray aircraft_->Cnfapf_aArray
2179 #define Cnfapf_pArray aircraft_->Cnfapf_pArray
2180 #define Cnfapf_CnArray aircraft_->Cnfapf_CnArray
2181 #define Cnfapf_nAlphaArray aircraft_->Cnfapf_nAlphaArray
2182 #define Cnfapf_np aircraft_->Cnfapf_np
2183 #define Cnfapf_fArray aircraft_->Cnfapf_fArray
2184 #define Cnfapf_nf aircraft_->Cnfapf_nf
2185 #define CnfapfI aircraft_->CnfapfI
2186 #define Cnfapf_nice aircraft_->Cnfapf_nice
2187 #define Cnfapf_na_nice aircraft_->Cnfapf_na_nice
2188 #define Cnfapf_np_nice aircraft_->Cnfapf_np_nice
2189 #define Cnfapf_pArray_nice aircraft_->Cnfapf_pArray_nice
2190 #define Cnfapf_aArray_nice aircraft_->Cnfapf_aArray_nice
2191 double Cnfarf_aArray[30][100][100];
2192 double Cnfarf_rArray[30][100];
2193 double Cnfarf_CnArray[30][100][100];
2194 int Cnfarf_nAlphaArray[30][100];
2196 double Cnfarf_fArray[30];
2199 int Cnfarf_nice, Cnfarf_na_nice, Cnfarf_nr_nice;
2200 double Cnfarf_rArray_nice[100];
2201 double Cnfarf_aArray_nice[100];
2202 #define Cnfarf_aArray aircraft_->Cnfarf_aArray
2203 #define Cnfarf_rArray aircraft_->Cnfarf_rArray
2204 #define Cnfarf_CnArray aircraft_->Cnfarf_CnArray
2205 #define Cnfarf_nAlphaArray aircraft_->Cnfarf_nAlphaArray
2206 #define Cnfarf_nr aircraft_->Cnfarf_nr
2207 #define Cnfarf_fArray aircraft_->Cnfarf_fArray
2208 #define Cnfarf_nf aircraft_->Cnfarf_nf
2209 #define CnfarfI aircraft_->CnfarfI
2210 #define Cnfarf_nice aircraft_->Cnfarf_nice
2211 #define Cnfarf_na_nice aircraft_->Cnfarf_na_nice
2212 #define Cnfarf_nr_nice aircraft_->Cnfarf_nr_nice
2213 #define Cnfarf_rArray_nice aircraft_->Cnfarf_rArray_nice
2214 #define Cnfarf_aArray_nice aircraft_->Cnfarf_aArray_nice
2215 double Cno_save, Cn_beta_save, Cn_p_save, Cn_r_save;
2216 double Cn_da_save, Cn_dr_save, Cn_q_save, Cn_b3_save;
2217 #define Cno_save aircraft_->Cno_save
2218 #define Cn_beta_save aircraft_->Cn_beta_save
2219 #define Cn_p_save aircraft_->Cn_p_save
2220 #define Cn_r_save aircraft_->Cn_r_save
2221 #define Cn_da_save aircraft_->Cn_da_save
2222 #define Cn_dr_save aircraft_->Cn_dr_save
2223 #define Cn_q_save aircraft_->Cn_q_save
2224 #define Cn_b3_save aircraft_->Cn_b3_save
2227 /* Variables (token2) ===========================================*/
2228 /* gear ========== Landing gear model quantities ================*/
2230 std::map <string,int> gear_map;
2232 #define gear_map aircraft_->gear_map
2234 bool gear_model[MAX_GEAR];
2235 SCALAR D_gear_v[MAX_GEAR][3];
2236 SCALAR cgear[MAX_GEAR];
2237 SCALAR kgear[MAX_GEAR];
2238 SCALAR muGear[MAX_GEAR];
2239 SCALAR strutLength[MAX_GEAR];
2240 #define D_gear_v aircraft_->D_gear_v
2241 #define gear_model aircraft_->gear_model
2242 #define cgear aircraft_->cgear
2243 #define kgear aircraft_->kgear
2244 #define muGear aircraft_->muGear
2245 #define strutLength aircraft_->strutLength
2246 double gear_max, gear_rate;
2247 #define gear_max aircraft_->gear_max
2248 #define gear_rate aircraft_->gear_rate
2250 #define use_gear aircraft_->use_gear
2253 /* Variables (token2) ===========================================*/
2254 /* ice =========== Ice model quantities ======================== */
2256 std::map <string,int> ice_map;
2257 #define ice_map aircraft_->ice_map
2259 bool ice_model, ice_on, beta_model;
2261 double transientTime;
2262 double eta_ice_final;
2264 double x_probe_wing;
2265 double x_probe_tail;
2266 #define ice_model aircraft_->ice_model
2267 #define ice_on aircraft_->ice_on
2268 #define beta_model aircraft_->beta_model
2269 #define iceTime aircraft_->iceTime
2270 #define transientTime aircraft_->transientTime
2271 #define eta_ice_final aircraft_->eta_ice_final
2272 #define eta_ice aircraft_->eta_ice
2273 #define x_probe_wing aircraft_->x_probe_wing
2274 #define x_probe_tail aircraft_->x_probe_tail
2275 double kCDo, kCDK, kCD_a, kCD_adot, kCD_q, kCD_de;
2276 double CDo_clean, CDK_clean, CD_a_clean, CD_adot_clean, CD_q_clean, CD_de_clean;
2277 #define kCDo aircraft_->kCDo
2278 #define kCDK aircraft_->kCDK
2279 #define kCD_a aircraft_->kCD_a
2280 #define kCD_adot aircraft_->kCD_adot
2281 #define kCD_q aircraft_->kCD_q
2282 #define kCD_de aircraft_->kCD_de
2283 #define CDo_clean aircraft_->CDo_clean
2284 #define CDK_clean aircraft_->CDK_clean
2285 #define CD_a_clean aircraft_->CD_a_clean
2286 #define CD_adot_clean aircraft_->CD_adot_clean
2287 #define CD_q_clean aircraft_->CD_q_clean
2288 #define CD_de_clean aircraft_->CD_de_clean
2289 double kCXo, kCXK, kCX_a, kCX_a2, kCX_a3, kCX_adot;
2290 double kCX_q, kCX_de, kCX_dr, kCX_df, kCX_adf;
2291 double CXo_clean, CXK_clean, CX_a_clean, CX_a2_clean, CX_a3_clean, CX_adot_clean;
2292 double CX_q_clean, CX_de_clean, CX_dr_clean, CX_df_clean, CX_adf_clean;
2293 #define kCXo aircraft_->kCXo
2294 #define kCXK aircraft_->kCXK
2295 #define kCX_a aircraft_->kCX_a
2296 #define kCX_a2 aircraft_->kCX_a2
2297 #define kCX_a3 aircraft_->kCX_a3
2298 #define kCX_adot aircraft_->kCX_adot
2299 #define kCX_q aircraft_->kCX_q
2300 #define kCX_de aircraft_->kCX_de
2301 #define kCX_dr aircraft_->kCX_dr
2302 #define kCX_df aircraft_->kCX_df
2303 #define kCX_adf aircraft_->kCX_adf
2304 #define CXo_clean aircraft_->CXo_clean
2305 #define CXK_clean aircraft_->CXK_clean
2306 #define CX_a_clean aircraft_->CX_a_clean
2307 #define CX_a2_clean aircraft_->CX_a2_clean
2308 #define CX_a3_clean aircraft_->CX_a3_clean
2309 #define CX_adot_clean aircraft_->CX_adot_clean
2310 #define CX_q_clean aircraft_->CX_q_clean
2311 #define CX_de_clean aircraft_->CX_de_clean
2312 #define CX_dr_clean aircraft_->CX_dr_clean
2313 #define CX_df_clean aircraft_->CX_df_clean
2314 #define CX_adf_clean aircraft_->CX_adf_clean
2315 double kCLo, kCL_a, kCL_adot, kCL_q, kCL_de;
2316 double CLo_clean, CL_a_clean, CL_adot_clean, CL_q_clean, CL_de_clean;
2317 #define kCLo aircraft_->kCLo
2318 #define kCL_a aircraft_->kCL_a
2319 #define kCL_adot aircraft_->kCL_adot
2320 #define kCL_q aircraft_->kCL_q
2321 #define kCL_de aircraft_->kCL_de
2322 #define CLo_clean aircraft_->CLo_clean
2323 #define CL_a_clean aircraft_->CL_a_clean
2324 #define CL_adot_clean aircraft_->CL_adot_clean
2325 #define CL_q_clean aircraft_->CL_q_clean
2326 #define CL_de_clean aircraft_->CL_de_clean
2327 double kCZo, kCZ_a, kCZ_a2, kCZ_a3, kCZ_adot, kCZ_q, kCZ_de, kCZ_deb2, kCZ_df, kCZ_adf;
2328 double CZo_clean, CZ_a_clean, CZ_a2_clean, CZ_a3_clean, CZ_adot_clean;
2329 double CZ_q_clean, CZ_de_clean, CZ_deb2_clean, CZ_df_clean, CZ_adf_clean;
2330 #define kCZo aircraft_->kCZo
2331 #define kCZ_a aircraft_->kCZ_a
2332 #define kCZ_a2 aircraft_->kCZ_a2
2333 #define kCZ_a3 aircraft_->kCZ_a3
2334 #define kCZ_adot aircraft_->kCZ_adot
2335 #define kCZ_q aircraft_->kCZ_q
2336 #define kCZ_de aircraft_->kCZ_de
2337 #define kCZ_deb2 aircraft_->kCZ_deb2
2338 #define kCZ_df aircraft_->kCZ_df
2339 #define kCZ_adf aircraft_->kCZ_adf
2340 #define CZo_clean aircraft_->CZo_clean
2341 #define CZ_a_clean aircraft_->CZ_a_clean
2342 #define CZ_a2_clean aircraft_->CZ_a2_clean
2343 #define CZ_a3_clean aircraft_->CZ_a3_clean
2344 #define CZ_adot_clean aircraft_->CZ_adot_clean
2345 #define CZ_q_clean aircraft_->CZ_q_clean
2346 #define CZ_de_clean aircraft_->CZ_de_clean
2347 #define CZ_deb2_clean aircraft_->CZ_deb2_clean
2348 #define CZ_df_clean aircraft_->CZ_df_clean
2349 #define CZ_adf_clean aircraft_->CZ_adf_clean
2350 double kCmo, kCm_a, kCm_a2, kCm_adot, kCm_q, kCm_de, kCm_b2, kCm_r, kCm_df;
2351 double Cmo_clean, Cm_a_clean, Cm_a2_clean, Cm_adot_clean, Cm_q_clean;
2352 double Cm_de_clean, Cm_b2_clean, Cm_r_clean, Cm_df_clean;
2353 #define kCmo aircraft_->kCmo
2354 #define kCm_a aircraft_->kCm_a
2355 #define kCm_a2 aircraft_->kCm_a2
2356 #define kCm_adot aircraft_->kCm_adot
2357 #define kCm_q aircraft_->kCm_q
2358 #define kCm_de aircraft_->kCm_de
2359 #define kCm_b2 aircraft_->kCm_b2
2360 #define kCm_r aircraft_->kCm_r
2361 #define kCm_df aircraft_->kCm_df
2362 #define Cmo_clean aircraft_->Cmo_clean
2363 #define Cm_a_clean aircraft_->Cm_a_clean
2364 #define Cm_a2_clean aircraft_->Cm_a2_clean
2365 #define Cm_adot_clean aircraft_->Cm_adot_clean
2366 #define Cm_q_clean aircraft_->Cm_q_clean
2367 #define Cm_de_clean aircraft_->Cm_de_clean
2368 #define Cm_b2_clean aircraft_->Cm_b2_clean
2369 #define Cm_r_clean aircraft_->Cm_r_clean
2370 #define Cm_df_clean aircraft_->Cm_df_clean
2371 double kCYo, kCY_beta, kCY_p, kCY_r, kCY_da, kCY_dr, kCY_dra, kCY_bdot;
2372 double CYo_clean, CY_beta_clean, CY_p_clean, CY_r_clean, CY_da_clean;
2373 double CY_dr_clean, CY_dra_clean, CY_bdot_clean;
2374 #define kCYo aircraft_->kCYo
2375 #define kCY_beta aircraft_->kCY_beta
2376 #define kCY_p aircraft_->kCY_p
2377 #define kCY_r aircraft_->kCY_r
2378 #define kCY_da aircraft_->kCY_da
2379 #define kCY_dr aircraft_->kCY_dr
2380 #define kCY_dra aircraft_->kCY_dra
2381 #define kCY_bdot aircraft_->kCY_bdot
2382 #define CYo_clean aircraft_->CYo_clean
2383 #define CY_beta_clean aircraft_->CY_beta_clean
2384 #define CY_p_clean aircraft_->CY_p_clean
2385 #define CY_r_clean aircraft_->CY_r_clean
2386 #define CY_da_clean aircraft_->CY_da_clean
2387 #define CY_dr_clean aircraft_->CY_dr_clean
2388 #define CY_dra_clean aircraft_->CY_dra_clean
2389 #define CY_bdot_clean aircraft_->CY_bdot_clean
2390 double kClo, kCl_beta, kCl_p, kCl_r, kCl_da, kCl_dr, kCl_daa;
2391 double Clo_clean, Cl_beta_clean, Cl_p_clean, Cl_r_clean, Cl_da_clean;
2392 double Cl_dr_clean, Cl_daa_clean;
2393 #define kClo aircraft_->kClo
2394 #define kCl_beta aircraft_->kCl_beta
2395 #define kCl_p aircraft_->kCl_p
2396 #define kCl_r aircraft_->kCl_r
2397 #define kCl_da aircraft_->kCl_da
2398 #define kCl_dr aircraft_->kCl_dr
2399 #define kCl_daa aircraft_->kCl_daa
2400 #define Clo_clean aircraft_->Clo_clean
2401 #define Cl_beta_clean aircraft_->Cl_beta_clean
2402 #define Cl_p_clean aircraft_->Cl_p_clean
2403 #define Cl_r_clean aircraft_->Cl_r_clean
2404 #define Cl_da_clean aircraft_->Cl_da_clean
2405 #define Cl_dr_clean aircraft_->Cl_dr_clean
2406 #define Cl_daa_clean aircraft_->Cl_daa_clean
2407 double kCno, kCn_beta, kCn_p, kCn_r, kCn_da, kCn_dr, kCn_q, kCn_b3;
2408 double Cno_clean, Cn_beta_clean, Cn_p_clean, Cn_r_clean, Cn_da_clean;
2409 double Cn_dr_clean, Cn_q_clean, Cn_b3_clean;
2410 #define kCno aircraft_->kCno
2411 #define kCn_beta aircraft_->kCn_beta
2412 #define kCn_p aircraft_->kCn_p
2413 #define kCn_r aircraft_->kCn_r
2414 #define kCn_da aircraft_->kCn_da
2415 #define kCn_dr aircraft_->kCn_dr
2416 #define kCn_q aircraft_->kCn_q
2417 #define kCn_b3 aircraft_->kCn_b3
2418 #define Cno_clean aircraft_->Cno_clean
2419 #define Cn_beta_clean aircraft_->Cn_beta_clean
2420 #define Cn_p_clean aircraft_->Cn_p_clean
2421 #define Cn_r_clean aircraft_->Cn_r_clean
2422 #define Cn_da_clean aircraft_->Cn_da_clean
2423 #define Cn_dr_clean aircraft_->Cn_dr_clean
2424 #define Cn_q_clean aircraft_->Cn_q_clean
2425 #define Cn_b3_clean aircraft_->Cn_b3_clean
2426 double bootTime[20];
2429 #define bootTime aircraft_->bootTime
2430 #define bootindex aircraft_->bootindex
2431 #define bootTrue aircraft_->bootTrue
2433 #define eta_from_file aircraft_->eta_from_file
2434 bool eta_wing_left_input;
2435 string eta_wing_left_input_file;
2436 double eta_wing_left_input_timeArray[100];
2437 double eta_wing_left_input_daArray[100];
2438 int eta_wing_left_input_ntime;
2439 double eta_wing_left_input_startTime;
2440 #define eta_wing_left_input aircraft_->eta_wing_left_input
2441 #define eta_wing_left_input_file aircraft_->eta_wing_left_input_file
2442 #define eta_wing_left_input_timeArray aircraft_->eta_wing_left_input_timeArray
2443 #define eta_wing_left_input_daArray aircraft_->eta_wing_left_input_daArray
2444 #define eta_wing_left_input_ntime aircraft_->eta_wing_left_input_ntime
2445 #define eta_wing_left_input_startTime aircraft_->eta_wing_left_input_startTime
2446 bool eta_wing_right_input;
2447 string eta_wing_right_input_file;
2448 double eta_wing_right_input_timeArray[100];
2449 double eta_wing_right_input_daArray[100];
2450 int eta_wing_right_input_ntime;
2451 double eta_wing_right_input_startTime;
2452 #define eta_wing_right_input aircraft_->eta_wing_right_input
2453 #define eta_wing_right_input_file aircraft_->eta_wing_right_input_file
2454 #define eta_wing_right_input_timeArray aircraft_->eta_wing_right_input_timeArray
2455 #define eta_wing_right_input_daArray aircraft_->eta_wing_right_input_daArray
2456 #define eta_wing_right_input_ntime aircraft_->eta_wing_right_input_ntime
2457 #define eta_wing_right_input_startTime aircraft_->eta_wing_right_input_startTime
2458 bool eta_tail_input;
2459 string eta_tail_input_file;
2460 double eta_tail_input_timeArray[100];
2461 double eta_tail_input_daArray[100];
2462 int eta_tail_input_ntime;
2463 double eta_tail_input_startTime;
2464 #define eta_tail_input aircraft_->eta_tail_input
2465 #define eta_tail_input_file aircraft_->eta_tail_input_file
2466 #define eta_tail_input_timeArray aircraft_->eta_tail_input_timeArray
2467 #define eta_tail_input_daArray aircraft_->eta_tail_input_daArray
2468 #define eta_tail_input_ntime aircraft_->eta_tail_input_ntime
2469 #define eta_tail_input_startTime aircraft_->eta_tail_input_startTime
2470 bool demo_eps_alpha_max;
2471 string demo_eps_alpha_max_file;
2472 double demo_eps_alpha_max_timeArray[100];
2473 double demo_eps_alpha_max_daArray[100];
2474 int demo_eps_alpha_max_ntime;
2475 double demo_eps_alpha_max_startTime;
2476 #define demo_eps_alpha_max aircraft_->demo_eps_alpha_max
2477 #define demo_eps_alpha_max_file aircraft_->demo_eps_alpha_max_file
2478 #define demo_eps_alpha_max_timeArray aircraft_->demo_eps_alpha_max_timeArray
2479 #define demo_eps_alpha_max_daArray aircraft_->demo_eps_alpha_max_daArray
2480 #define demo_eps_alpha_max_ntime aircraft_->demo_eps_alpha_max_ntime
2481 #define demo_eps_alpha_max_startTime aircraft_->demo_eps_alpha_max_startTime
2482 bool demo_eps_pitch_max;
2483 string demo_eps_pitch_max_file;
2484 double demo_eps_pitch_max_timeArray[100];
2485 double demo_eps_pitch_max_daArray[100];
2486 int demo_eps_pitch_max_ntime;
2487 double demo_eps_pitch_max_startTime;
2488 #define demo_eps_pitch_max aircraft_->demo_eps_pitch_max
2489 #define demo_eps_pitch_max_file aircraft_->demo_eps_pitch_max_file
2490 #define demo_eps_pitch_max_timeArray aircraft_->demo_eps_pitch_max_timeArray
2491 #define demo_eps_pitch_max_daArray aircraft_->demo_eps_pitch_max_daArray
2492 #define demo_eps_pitch_max_ntime aircraft_->demo_eps_pitch_max_ntime
2493 #define demo_eps_pitch_max_startTime aircraft_->demo_eps_pitch_max_startTime
2494 bool demo_eps_pitch_min;
2495 string demo_eps_pitch_min_file;
2496 double demo_eps_pitch_min_timeArray[100];
2497 double demo_eps_pitch_min_daArray[100];
2498 int demo_eps_pitch_min_ntime;
2499 double demo_eps_pitch_min_startTime;
2500 #define demo_eps_pitch_min aircraft_->demo_eps_pitch_min
2501 #define demo_eps_pitch_min_file aircraft_->demo_eps_pitch_min_file
2502 #define demo_eps_pitch_min_timeArray aircraft_->demo_eps_pitch_min_timeArray
2503 #define demo_eps_pitch_min_daArray aircraft_->demo_eps_pitch_min_daArray
2504 #define demo_eps_pitch_min_ntime aircraft_->demo_eps_pitch_min_ntime
2505 #define demo_eps_pitch_min_startTime aircraft_->demo_eps_pitch_min_startTime
2506 bool demo_eps_roll_max;
2507 string demo_eps_roll_max_file;
2508 double demo_eps_roll_max_timeArray[10];
2509 double demo_eps_roll_max_daArray[10];
2510 int demo_eps_roll_max_ntime;
2511 double demo_eps_roll_max_startTime;
2512 #define demo_eps_roll_max aircraft_->demo_eps_roll_max
2513 #define demo_eps_roll_max_file aircraft_->demo_eps_roll_max_file
2514 #define demo_eps_roll_max_timeArray aircraft_->demo_eps_roll_max_timeArray
2515 #define demo_eps_roll_max_daArray aircraft_->demo_eps_roll_max_daArray
2516 #define demo_eps_roll_max_ntime aircraft_->demo_eps_roll_max_ntime
2517 #define demo_eps_roll_max_startTime aircraft_->demo_eps_roll_max_startTime
2518 bool demo_eps_thrust_min;
2519 string demo_eps_thrust_min_file;
2520 double demo_eps_thrust_min_timeArray[100];
2521 double demo_eps_thrust_min_daArray[100];
2522 int demo_eps_thrust_min_ntime;
2523 double demo_eps_thrust_min_startTime;
2524 #define demo_eps_thrust_min aircraft_->demo_eps_thrust_min
2525 #define demo_eps_thrust_min_file aircraft_->demo_eps_thrust_min_file
2526 #define demo_eps_thrust_min_timeArray aircraft_->demo_eps_thrust_min_timeArray
2527 #define demo_eps_thrust_min_daArray aircraft_->demo_eps_thrust_min_daArray
2528 #define demo_eps_thrust_min_ntime aircraft_->demo_eps_thrust_min_ntime
2529 #define demo_eps_thrust_min_startTime aircraft_->demo_eps_thrust_min_startTime
2530 bool demo_eps_airspeed_max;
2531 string demo_eps_airspeed_max_file;
2532 double demo_eps_airspeed_max_timeArray[10];
2533 double demo_eps_airspeed_max_daArray[10];
2534 int demo_eps_airspeed_max_ntime;
2535 double demo_eps_airspeed_max_startTime;
2536 #define demo_eps_airspeed_max aircraft_->demo_eps_airspeed_max
2537 #define demo_eps_airspeed_max_file aircraft_->demo_eps_airspeed_max_file
2538 #define demo_eps_airspeed_max_timeArray aircraft_->demo_eps_airspeed_max_timeArray
2539 #define demo_eps_airspeed_max_daArray aircraft_->demo_eps_airspeed_max_daArray
2540 #define demo_eps_airspeed_max_ntime aircraft_->demo_eps_airspeed_max_ntime
2541 #define demo_eps_airspeed_max_startTime aircraft_->demo_eps_airspeed_max_startTime
2542 bool demo_eps_airspeed_min;
2543 string demo_eps_airspeed_min_file;
2544 double demo_eps_airspeed_min_timeArray[100];
2545 double demo_eps_airspeed_min_daArray[100];
2546 int demo_eps_airspeed_min_ntime;
2547 double demo_eps_airspeed_min_startTime;
2548 #define demo_eps_airspeed_min aircraft_->demo_eps_airspeed_min
2549 #define demo_eps_airspeed_min_file aircraft_->demo_eps_airspeed_min_file
2550 #define demo_eps_airspeed_min_timeArray aircraft_->demo_eps_airspeed_min_timeArray
2551 #define demo_eps_airspeed_min_daArray aircraft_->demo_eps_airspeed_min_daArray
2552 #define demo_eps_airspeed_min_ntime aircraft_->demo_eps_airspeed_min_ntime
2553 #define demo_eps_airspeed_min_startTime aircraft_->demo_eps_airspeed_min_startTime
2554 bool demo_eps_flap_max;
2555 string demo_eps_flap_max_file;
2556 double demo_eps_flap_max_timeArray[10];
2557 double demo_eps_flap_max_daArray[10];
2558 int demo_eps_flap_max_ntime;
2559 double demo_eps_flap_max_startTime;
2560 #define demo_eps_flap_max aircraft_->demo_eps_flap_max
2561 #define demo_eps_flap_max_file aircraft_->demo_eps_flap_max_file
2562 #define demo_eps_flap_max_timeArray aircraft_->demo_eps_flap_max_timeArray
2563 #define demo_eps_flap_max_daArray aircraft_->demo_eps_flap_max_daArray
2564 #define demo_eps_flap_max_ntime aircraft_->demo_eps_flap_max_ntime
2565 #define demo_eps_flap_max_startTime aircraft_->demo_eps_flap_max_startTime
2566 bool demo_boot_cycle_tail;
2567 string demo_boot_cycle_tail_file;
2568 double demo_boot_cycle_tail_timeArray[100];
2569 int demo_boot_cycle_tail_daArray[100];
2570 int demo_boot_cycle_tail_ntime;
2571 double demo_boot_cycle_tail_startTime;
2572 #define demo_boot_cycle_tail aircraft_->demo_boot_cycle_tail
2573 #define demo_boot_cycle_tail_file aircraft_->demo_boot_cycle_tail_file
2574 #define demo_boot_cycle_tail_timeArray aircraft_->demo_boot_cycle_tail_timeArray
2575 #define demo_boot_cycle_tail_daArray aircraft_->demo_boot_cycle_tail_daArray
2576 #define demo_boot_cycle_tail_ntime aircraft_->demo_boot_cycle_tail_ntime
2577 #define demo_boot_cycle_tail_startTime aircraft_->demo_boot_cycle_tail_startTime
2578 bool demo_boot_cycle_wing_left;
2579 string demo_boot_cycle_wing_left_file;
2580 double demo_boot_cycle_wing_left_timeArray[100];
2581 int demo_boot_cycle_wing_left_daArray[100];
2582 int demo_boot_cycle_wing_left_ntime;
2583 double demo_boot_cycle_wing_left_startTime;
2584 #define demo_boot_cycle_wing_left aircraft_->demo_boot_cycle_wing_left
2585 #define demo_boot_cycle_wing_left_file aircraft_->demo_boot_cycle_wing_left_file
2586 #define demo_boot_cycle_wing_left_timeArray aircraft_->demo_boot_cycle_wing_left_timeArray
2587 #define demo_boot_cycle_wing_left_daArray aircraft_->demo_boot_cycle_wing_left_daArray
2588 #define demo_boot_cycle_wing_left_ntime aircraft_->demo_boot_cycle_wing_left_ntime
2589 #define demo_boot_cycle_wing_left_startTime aircraft_->demo_boot_cycle_wing_left_startTime
2590 bool demo_boot_cycle_wing_right;
2591 string demo_boot_cycle_wing_right_file;
2592 double demo_boot_cycle_wing_right_timeArray[100];
2593 int demo_boot_cycle_wing_right_daArray[100];
2594 int demo_boot_cycle_wing_right_ntime;
2595 double demo_boot_cycle_wing_right_startTime;
2596 #define demo_boot_cycle_wing_right aircraft_->demo_boot_cycle_wing_right
2597 #define demo_boot_cycle_wing_right_file aircraft_->demo_boot_cycle_wing_right_file
2598 #define demo_boot_cycle_wing_right_timeArray aircraft_->demo_boot_cycle_wing_right_timeArray
2599 #define demo_boot_cycle_wing_right_daArray aircraft_->demo_boot_cycle_wing_right_daArray
2600 #define demo_boot_cycle_wing_right_ntime aircraft_->demo_boot_cycle_wing_right_ntime
2601 #define demo_boot_cycle_wing_right_startTime aircraft_->demo_boot_cycle_wing_right_startTime
2602 bool demo_eps_pitch_input;
2603 string demo_eps_pitch_input_file;
2604 double demo_eps_pitch_input_timeArray[100];
2605 int demo_eps_pitch_input_daArray[100];
2606 int demo_eps_pitch_input_ntime;
2607 double demo_eps_pitch_input_startTime;
2608 #define demo_eps_pitch_input aircraft_->demo_eps_pitch_input
2609 #define demo_eps_pitch_input_file aircraft_->demo_eps_pitch_input_file
2610 #define demo_eps_pitch_input_timeArray aircraft_->demo_eps_pitch_input_timeArray
2611 #define demo_eps_pitch_input_daArray aircraft_->demo_eps_pitch_input_daArray
2612 #define demo_eps_pitch_input_ntime aircraft_->demo_eps_pitch_input_ntime
2613 #define demo_eps_pitch_input_startTime aircraft_->demo_eps_pitch_input_startTime
2615 double tactilefadef_aArray[30][100][100];
2616 double tactilefadef_deArray[30][100];
2617 double tactilefadef_tactileArray[30][100][100];
2618 int tactilefadef_nAlphaArray[30][100];
2619 int tactilefadef_nde[30];
2620 double tactilefadef_fArray[30];
2621 int tactilefadef_nf;
2622 double tactilefadefI;
2623 int tactilefadef_nice, tactilefadef_na_nice, tactilefadef_nde_nice;
2624 double tactilefadef_deArray_nice[100];
2625 double tactilefadef_aArray_nice[100];
2626 #define tactilefadef aircraft_->tactilefadef
2627 #define tactilefadef_aArray aircraft_->tactilefadef_aArray
2628 #define tactilefadef_deArray aircraft_->tactilefadef_deArray
2629 #define tactilefadef_tactileArray aircraft_->tactilefadef_tactileArray
2630 #define tactilefadef_nAlphaArray aircraft_->tactilefadef_nAlphaArray
2631 #define tactilefadef_nde aircraft_->tactilefadef_nde
2632 #define tactilefadef_fArray aircraft_->tactilefadef_fArray
2633 #define tactilefadef_nf aircraft_->tactilefadef_nf
2634 #define tactilefadefI aircraft_->tactilefadefI
2635 #define tactilefadef_nice aircraft_->tactilefadef_nice
2636 #define tactilefadef_na_nice aircraft_->tactilefadef_na_nice
2637 #define tactilefadef_nde_nice aircraft_->tactilefadef_nde_nice
2638 #define tactilefadef_deArray_nice aircraft_->tactilefadef_deArray_nice
2639 #define tactilefadef_aArray_nice aircraft_->tactilefadef_aArray_nice
2641 #define tactile_pitch aircraft_->tactile_pitch
2642 bool demo_ap_pah_on;
2643 string demo_ap_pah_on_file;
2644 double demo_ap_pah_on_timeArray[10];
2645 int demo_ap_pah_on_daArray[10];
2646 int demo_ap_pah_on_ntime;
2647 double demo_ap_pah_on_startTime;
2648 #define demo_ap_pah_on aircraft_->demo_ap_pah_on
2649 #define demo_ap_pah_on_file aircraft_->demo_ap_pah_on_file
2650 #define demo_ap_pah_on_timeArray aircraft_->demo_ap_pah_on_timeArray
2651 #define demo_ap_pah_on_daArray aircraft_->demo_ap_pah_on_daArray
2652 #define demo_ap_pah_on_ntime aircraft_->demo_ap_pah_on_ntime
2653 #define demo_ap_pah_on_startTime aircraft_->demo_ap_pah_on_startTime
2654 bool demo_ap_alh_on;
2655 string demo_ap_alh_on_file;
2656 double demo_ap_alh_on_timeArray[10];
2657 int demo_ap_alh_on_daArray[10];
2658 int demo_ap_alh_on_ntime;
2659 double demo_ap_alh_on_startTime;
2660 #define demo_ap_alh_on aircraft_->demo_ap_alh_on
2661 #define demo_ap_alh_on_file aircraft_->demo_ap_alh_on_file
2662 #define demo_ap_alh_on_timeArray aircraft_->demo_ap_alh_on_timeArray
2663 #define demo_ap_alh_on_daArray aircraft_->demo_ap_alh_on_daArray
2664 #define demo_ap_alh_on_ntime aircraft_->demo_ap_alh_on_ntime
2665 #define demo_ap_alh_on_startTime aircraft_->demo_ap_alh_on_startTime
2666 bool demo_ap_rah_on;
2667 string demo_ap_rah_on_file;
2668 double demo_ap_rah_on_timeArray[10];
2669 int demo_ap_rah_on_daArray[10];
2670 int demo_ap_rah_on_ntime;
2671 double demo_ap_rah_on_startTime;
2672 #define demo_ap_rah_on aircraft_->demo_ap_rah_on
2673 #define demo_ap_rah_on_file aircraft_->demo_ap_rah_on_file
2674 #define demo_ap_rah_on_timeArray aircraft_->demo_ap_rah_on_timeArray
2675 #define demo_ap_rah_on_daArray aircraft_->demo_ap_rah_on_daArray
2676 #define demo_ap_rah_on_ntime aircraft_->demo_ap_rah_on_ntime
2677 #define demo_ap_rah_on_startTime aircraft_->demo_ap_rah_on_startTime
2679 string demo_ap_hh_on_file;
2680 double demo_ap_hh_on_timeArray[10];
2681 int demo_ap_hh_on_daArray[10];
2682 int demo_ap_hh_on_ntime;
2683 double demo_ap_hh_on_startTime;
2684 #define demo_ap_hh_on aircraft_->demo_ap_hh_on
2685 #define demo_ap_hh_on_file aircraft_->demo_ap_hh_on_file
2686 #define demo_ap_hh_on_timeArray aircraft_->demo_ap_hh_on_timeArray
2687 #define demo_ap_hh_on_daArray aircraft_->demo_ap_hh_on_daArray
2688 #define demo_ap_hh_on_ntime aircraft_->demo_ap_hh_on_ntime
2689 #define demo_ap_hh_on_startTime aircraft_->demo_ap_hh_on_startTime
2690 bool demo_ap_Theta_ref;
2691 string demo_ap_Theta_ref_file;
2692 double demo_ap_Theta_ref_timeArray[10];
2693 double demo_ap_Theta_ref_daArray[10];
2694 int demo_ap_Theta_ref_ntime;
2695 double demo_ap_Theta_ref_startTime;
2696 #define demo_ap_Theta_ref aircraft_->demo_ap_Theta_ref
2697 #define demo_ap_Theta_ref_file aircraft_->demo_ap_Theta_ref_file
2698 #define demo_ap_Theta_ref_timeArray aircraft_->demo_ap_Theta_ref_timeArray
2699 #define demo_ap_Theta_ref_daArray aircraft_->demo_ap_Theta_ref_daArray
2700 #define demo_ap_Theta_ref_ntime aircraft_->demo_ap_Theta_ref_ntime
2701 #define demo_ap_Theta_ref_startTime aircraft_->demo_ap_Theta_ref_startTime
2702 bool demo_ap_alt_ref;
2703 string demo_ap_alt_ref_file;
2704 double demo_ap_alt_ref_timeArray[10];
2705 double demo_ap_alt_ref_daArray[10];
2706 int demo_ap_alt_ref_ntime;
2707 double demo_ap_alt_ref_startTime;
2708 #define demo_ap_alt_ref aircraft_->demo_ap_alt_ref
2709 #define demo_ap_alt_ref_file aircraft_->demo_ap_alt_ref_file
2710 #define demo_ap_alt_ref_timeArray aircraft_->demo_ap_alt_ref_timeArray
2711 #define demo_ap_alt_ref_daArray aircraft_->demo_ap_alt_ref_daArray
2712 #define demo_ap_alt_ref_ntime aircraft_->demo_ap_alt_ref_ntime
2713 #define demo_ap_alt_ref_startTime aircraft_->demo_ap_alt_ref_startTime
2714 bool demo_ap_Phi_ref;
2715 string demo_ap_Phi_ref_file;
2716 double demo_ap_Phi_ref_timeArray[10];
2717 double demo_ap_Phi_ref_daArray[10];
2718 int demo_ap_Phi_ref_ntime;
2719 double demo_ap_Phi_ref_startTime;
2720 #define demo_ap_Phi_ref aircraft_->demo_ap_Phi_ref
2721 #define demo_ap_Phi_ref_file aircraft_->demo_ap_Phi_ref_file
2722 #define demo_ap_Phi_ref_timeArray aircraft_->demo_ap_Phi_ref_timeArray
2723 #define demo_ap_Phi_ref_daArray aircraft_->demo_ap_Phi_ref_daArray
2724 #define demo_ap_Phi_ref_ntime aircraft_->demo_ap_Phi_ref_ntime
2725 #define demo_ap_Phi_ref_startTime aircraft_->demo_ap_Phi_ref_startTime
2726 bool demo_ap_Psi_ref;
2727 string demo_ap_Psi_ref_file;
2728 double demo_ap_Psi_ref_timeArray[10];
2729 double demo_ap_Psi_ref_daArray[10];
2730 int demo_ap_Psi_ref_ntime;
2731 double demo_ap_Psi_ref_startTime;
2732 #define demo_ap_Psi_ref aircraft_->demo_ap_Psi_ref
2733 #define demo_ap_Psi_ref_file aircraft_->demo_ap_Psi_ref_file
2734 #define demo_ap_Psi_ref_timeArray aircraft_->demo_ap_Psi_ref_timeArray
2735 #define demo_ap_Psi_ref_daArray aircraft_->demo_ap_Psi_ref_daArray
2736 #define demo_ap_Psi_ref_ntime aircraft_->demo_ap_Psi_ref_ntime
2737 #define demo_ap_Psi_ref_startTime aircraft_->demo_ap_Psi_ref_startTime
2739 string demo_tactile_file;
2740 double demo_tactile_timeArray[1500];
2741 double demo_tactile_daArray[1500];
2742 int demo_tactile_ntime;
2743 double demo_tactile_startTime;
2744 #define demo_tactile aircraft_->demo_tactile
2745 #define demo_tactile_file aircraft_->demo_tactile_file
2746 #define demo_tactile_timeArray aircraft_->demo_tactile_timeArray
2747 #define demo_tactile_daArray aircraft_->demo_tactile_daArray
2748 #define demo_tactile_ntime aircraft_->demo_tactile_ntime
2749 #define demo_tactile_startTime aircraft_->demo_tactile_startTime
2751 string demo_ice_tail_file;
2752 double demo_ice_tail_timeArray[10];
2753 int demo_ice_tail_daArray[10];
2754 int demo_ice_tail_ntime;
2755 double demo_ice_tail_startTime;
2756 #define demo_ice_tail aircraft_->demo_ice_tail
2757 #define demo_ice_tail_file aircraft_->demo_ice_tail_file
2758 #define demo_ice_tail_timeArray aircraft_->demo_ice_tail_timeArray
2759 #define demo_ice_tail_daArray aircraft_->demo_ice_tail_daArray
2760 #define demo_ice_tail_ntime aircraft_->demo_ice_tail_ntime
2761 #define demo_ice_tail_startTime aircraft_->demo_ice_tail_startTime
2763 string demo_ice_left_file;
2764 double demo_ice_left_timeArray[10];
2765 int demo_ice_left_daArray[10];
2766 int demo_ice_left_ntime;
2767 double demo_ice_left_startTime;
2768 #define demo_ice_left aircraft_->demo_ice_left
2769 #define demo_ice_left_file aircraft_->demo_ice_left_file
2770 #define demo_ice_left_timeArray aircraft_->demo_ice_left_timeArray
2771 #define demo_ice_left_daArray aircraft_->demo_ice_left_daArray
2772 #define demo_ice_left_ntime aircraft_->demo_ice_left_ntime
2773 #define demo_ice_left_startTime aircraft_->demo_ice_left_startTime
2774 bool demo_ice_right;
2775 string demo_ice_right_file;
2776 double demo_ice_right_timeArray[10];
2777 int demo_ice_right_daArray[10];
2778 int demo_ice_right_ntime;
2779 double demo_ice_right_startTime;
2780 #define demo_ice_right aircraft_->demo_ice_right
2781 #define demo_ice_right_file aircraft_->demo_ice_right_file
2782 #define demo_ice_right_timeArray aircraft_->demo_ice_right_timeArray
2783 #define demo_ice_right_daArray aircraft_->demo_ice_right_daArray
2784 #define demo_ice_right_ntime aircraft_->demo_ice_right_ntime
2785 #define demo_ice_right_startTime aircraft_->demo_ice_right_startTime
2788 /* Variables (token2) ===========================================*/
2789 /* fog =========== Fog field quantities ======================== */
2791 std::map <string,int> fog_map;
2792 #define fog_map aircraft_->fog_map
2796 int fog_point_index;
2799 double fog_next_time;
2800 int fog_current_segment;
2804 #define fog_field aircraft_->fog_field
2805 #define fog_segments aircraft_->fog_segments
2806 #define fog_point_index aircraft_->fog_point_index
2807 #define fog_time aircraft_->fog_time
2808 #define fog_value aircraft_->fog_value
2809 #define fog_next_time aircraft_->fog_next_time
2810 #define fog_current_segment aircraft_->fog_current_segment
2812 #define Fog aircraft_->Fog
2816 /* Variables (token2) ===========================================*/
2817 /* record ======== Record desired quantites to file =============*/
2819 std::map <string,int> record_map;
2820 #define record_map aircraft_->record_map
2822 /***** Angles ******/
2823 double Alpha_deg, Alpha_dot_deg, Beta_deg, Beta_dot_deg;
2824 #define Alpha_deg aircraft_->Alpha_deg
2825 #define Alpha_dot_deg aircraft_->Alpha_dot_deg
2826 #define Beta_deg aircraft_->Beta_deg
2827 #define Beta_dot_deg aircraft_->Beta_dot_deg
2828 double Gamma_vert_deg, Gamma_horiz_deg;
2829 #define Gamma_vert_deg aircraft_->Gamma_vert_deg
2830 #define Gamma_horiz_deg aircraft_->Gamma_horiz_deg
2832 /** Control Inputs **/
2833 double Long_trim_deg, elevator_tab, elevator_deg, aileron_deg, rudder_deg;
2834 #define Long_trim_deg aircraft_->Long_trim_deg
2835 #define elevator_tab aircraft_->elevator_tab
2836 #define elevator_deg aircraft_->elevator_deg
2837 #define aileron_deg aircraft_->aileron_deg
2838 #define rudder_deg aircraft_->rudder_deg
2839 // double flap_pos_deg;
2840 //#define flap_pos_deg aircraft_->flap_pos_deg
2842 /***** Forces ******/
2843 double F_X_wind, F_Y_wind, F_Z_wind;
2844 #define F_X_wind aircraft_->F_X_wind
2845 #define F_Y_wind aircraft_->F_Y_wind
2846 #define F_Z_wind aircraft_->F_Z_wind
2847 double Lift_clean_wing, Lift_iced_wing;
2848 double Lift_clean_tail, Lift_iced_tail;
2849 #define Lift_clean_wing aircraft_->Lift_clean_wing
2850 #define Lift_iced_wing aircraft_->Lift_iced_wing
2851 #define Lift_clean_tail aircraft_->Lift_clean_tail
2852 #define Lift_iced_tail aircraft_->Lift_iced_tail
2853 double Gamma_clean_wing, Gamma_iced_wing;
2854 double Gamma_clean_tail, Gamma_iced_tail;
2855 #define Gamma_clean_wing aircraft_->Gamma_clean_wing
2856 #define Gamma_iced_wing aircraft_->Gamma_iced_wing
2857 #define Gamma_clean_tail aircraft_->Gamma_clean_tail
2858 #define Gamma_iced_tail aircraft_->Gamma_iced_tail
2859 double w_clean_wing, w_iced_wing;
2860 double w_clean_tail, w_iced_tail;
2861 #define w_clean_wing aircraft_->w_clean_wing
2862 #define w_iced_wing aircraft_->w_iced_wing
2863 #define w_clean_tail aircraft_->w_clean_tail
2864 #define w_iced_tail aircraft_->w_iced_tail
2865 double V_total_clean_wing, V_total_iced_wing;
2866 double V_total_clean_tail, V_total_iced_tail;
2867 #define V_total_clean_wing aircraft_->V_total_clean_wing
2868 #define V_total_iced_wing aircraft_->V_total_iced_wing
2869 #define V_total_clean_tail aircraft_->V_total_clean_tail
2870 #define V_total_iced_tail aircraft_->V_total_iced_tail
2871 double beta_flow_clean_wing, beta_flow_clean_wing_deg;
2872 double beta_flow_iced_wing, beta_flow_iced_wing_deg;
2873 double beta_flow_clean_tail, beta_flow_clean_tail_deg;
2874 double beta_flow_iced_tail, beta_flow_iced_tail_deg;
2875 #define beta_flow_clean_wing aircraft_->beta_flow_clean_wing
2876 #define beta_flow_clean_wing_deg aircraft_->beta_flow_clean_wing_deg
2877 #define beta_flow_iced_wing aircraft_->beta_flow_iced_wing
2878 #define beta_flow_iced_wing_deg aircraft_->beta_flow_iced_wing_deg
2879 #define beta_flow_clean_tail aircraft_->beta_flow_clean_tail
2880 #define beta_flow_clean_tail_deg aircraft_->beta_flow_clean_tail_deg
2881 #define beta_flow_iced_tail aircraft_->beta_flow_iced_tail
2882 #define beta_flow_iced_tail_deg aircraft_->beta_flow_iced_tail_deg
2883 double Dbeta_flow_wing, Dbeta_flow_wing_deg;
2884 double Dbeta_flow_tail, Dbeta_flow_tail_deg;
2885 #define Dbeta_flow_wing aircraft_->Dbeta_flow_wing
2886 #define Dbeta_flow_wing_deg aircraft_->Dbeta_flow_wing_deg
2887 #define Dbeta_flow_tail aircraft_->Dbeta_flow_tail
2888 #define Dbeta_flow_tail_deg aircraft_->Dbeta_flow_tail_deg
2889 double pct_beta_flow_wing, pct_beta_flow_tail;
2890 #define pct_beta_flow_wing aircraft_->pct_beta_flow_wing
2891 #define pct_beta_flow_tail aircraft_->pct_beta_flow_tail
2894 /* Variables (token2) ===========================================*/
2895 /* misc ========== Miscellaneous input commands =================*/
2897 std::map <string,int> misc_map;
2898 #define misc_map aircraft_->misc_map
2900 double simpleHingeMomentCoef;
2901 #define simpleHingeMomentCoef aircraft_->simpleHingeMomentCoef
2903 //double dfTimefdf_dfArray[100];
2904 //double dfTimefdf_TimeArray[100];
2905 //int dfTimefdf_ndf;
2906 //#define dfTimefdf aircraft_->dfTimefdf
2907 //#define dfTimefdf_dfArray aircraft_->dfTimefdf_dfArray
2908 //#define dfTimefdf_TimeArray aircraft_->dfTimefdf_TimeArray
2909 //#define dfTimefdf_ndf aircraft_->dfTimefdf_ndf
2911 FlapData *flapper_data;
2912 #define flapper_data aircraft_->flapper_data
2914 #define flapper_model aircraft_->flapper_model
2915 double flapper_phi_init;
2916 #define flapper_phi_init aircraft_->flapper_phi_init
2917 double flapper_freq, flapper_cycle_pct, flapper_phi;
2918 double flapper_Lift, flapper_Thrust, flapper_Inertia;
2919 double flapper_Moment;
2920 #define flapper_freq aircraft_->flapper_freq
2921 #define flapper_cycle_pct aircraft_->flapper_cycle_pct
2922 #define flapper_phi aircraft_->flapper_phi
2923 #define flapper_Lift aircraft_->flapper_Lift
2924 #define flapper_Thrust aircraft_->flapper_Thrust
2925 #define flapper_Inertia aircraft_->flapper_Inertia
2926 #define flapper_Moment aircraft_->flapper_Moment
2927 double F_X_aero_flapper, F_Z_aero_flapper;
2928 #define F_X_aero_flapper aircraft_->F_X_aero_flapper
2929 #define F_Z_aero_flapper aircraft_->F_Z_aero_flapper
2931 /* Other variables (not tokens) =================================*/
2933 double convert_x, convert_y, convert_z;
2934 #define convert_x aircraft_->convert_x
2935 #define convert_y aircraft_->convert_y
2936 #define convert_z aircraft_->convert_z
2938 double cbar_2U, b_2U, ch_2U;
2939 #define cbar_2U aircraft_->cbar_2U
2940 #define b_2U aircraft_->b_2U
2941 #define ch_2U aircraft_->ch_2U
2944 double dfArray[100];
2945 double TimeArray[100];
2946 #define ndf aircraft_->ndf
2947 #define dfArray aircraft_->dfArray
2948 #define TimeArray aircraft_->TimeArray
2950 double flap_percent, flap_increment_per_timestep, flap_cmd, flap_pos, flap_pos_norm;
2951 #define flap_percent aircraft_->flap_percent
2952 #define flap_increment_per_timestep aircraft_->flap_increment_per_timestep
2953 #define flap_cmd aircraft_->flap_cmd
2954 #define flap_pos aircraft_->flap_pos
2955 #define flap_pos_norm aircraft_->flap_pos_norm
2957 double Spoiler_handle, spoiler_increment_per_timestep, spoiler_cmd;
2958 double spoiler_pos_norm, spoiler_pos;
2959 #define Spoiler_handle aircraft_->Spoiler_handle
2960 #define spoiler_increment_per_timestep aircraft_->spoiler_increment_per_timestep
2961 #define spoiler_cmd aircraft_->spoiler_cmd
2962 #define spoiler_pos_norm aircraft_->spoiler_pos_norm
2963 #define spoiler_pos aircraft_->spoiler_pos
2965 double Gear_handle, gear_increment_per_timestep, gear_cmd_norm, gear_pos_norm;
2966 #define Gear_handle aircraft_->Gear_handle
2967 #define gear_increment_per_timestep aircraft_->gear_increment_per_timestep
2968 #define gear_cmd_norm aircraft_->gear_cmd_norm
2969 #define gear_pos_norm aircraft_->gear_pos_norm
2971 double delta_CL, delta_CD, delta_Cm, delta_Ch, delta_Cl, delta_Cn;
2972 #define delta_CL aircraft_->delta_CL
2973 #define delta_CD aircraft_->delta_CD
2974 #define delta_Cm aircraft_->delta_Cm
2975 #define delta_Ch aircraft_->delta_Ch
2976 #define delta_Cl aircraft_->delta_Cl
2977 #define delta_Cn aircraft_->delta_Cn
2979 int nonlin_ice_case;
2980 double eta_wing_left, eta_wing_right, eta_tail;
2981 double OATemperature_F;
2982 #define nonlin_ice_case aircraft_->nonlin_ice_case
2983 #define eta_wing_left aircraft_->eta_wing_left
2984 #define eta_wing_right aircraft_->eta_wing_right
2985 #define eta_tail aircraft_->eta_tail
2986 #define OATemperature_F aircraft_->OATemperature_F
2987 int boot_cycle_tail, boot_cycle_wing_left, boot_cycle_wing_right;
2988 int autoIPS_tail, autoIPS_wing_left, autoIPS_wing_right;
2989 int eps_pitch_input;
2990 double eps_alpha_max, eps_pitch_max, eps_pitch_min;
2991 double eps_roll_max, eps_thrust_min, eps_flap_max;
2992 double eps_airspeed_max, eps_airspeed_min;
2993 #define boot_cycle_tail aircraft_->boot_cycle_tail
2994 #define boot_cycle_wing_left aircraft_->boot_cycle_wing_left
2995 #define boot_cycle_wing_right aircraft_->boot_cycle_wing_right
2996 #define autoIPS_tail aircraft_->autoIPS_tail
2997 #define autoIPS_wing_left aircraft_->autoIPS_wing_left
2998 #define autoIPS_wing_right aircraft_->autoIPS_wing_right
2999 #define eps_pitch_input aircraft_->eps_pitch_input
3000 #define eps_alpha_max aircraft_->eps_alpha_max
3001 #define eps_pitch_max aircraft_->eps_pitch_max
3002 #define eps_pitch_min aircraft_->eps_pitch_min
3003 #define eps_roll_max aircraft_->eps_roll_max
3004 #define eps_thrust_min aircraft_->eps_thrust_min
3005 #define eps_flap_max aircraft_->eps_flap_max
3006 #define eps_airspeed_max aircraft_->eps_airspeed_max
3007 #define eps_airspeed_min aircraft_->eps_airspeed_min
3010 #define Ch aircraft_->Ch;
3012 double CL_clean, CL_iced;
3013 double CY_clean, CY_iced;
3014 double CD_clean, CD_iced;
3015 double Cm_clean, Cm_iced;
3016 double Cl_clean, Cl_iced;
3017 double Cn_clean, Cn_iced;
3018 double Ch_clean, Ch_iced;
3019 #define CL_clean aircraft_->CL_clean
3020 #define CY_clean aircraft_->CY_clean
3021 #define CD_clean aircraft_->CD_clean
3022 #define Cm_clean aircraft_->Cm_clean
3023 #define Cl_clean aircraft_->Cl_clean
3024 #define Cn_clean aircraft_->Cn_clean
3025 #define Ch_clean aircraft_->Ch_clean
3026 #define CL_iced aircraft_->CL_iced
3027 #define CY_iced aircraft_->CY_iced
3028 #define CD_iced aircraft_->CD_iced
3029 #define Cm_iced aircraft_->Cm_iced
3030 #define Cl_iced aircraft_->Cl_iced
3031 #define Cn_iced aircraft_->Cn_iced
3032 #define Ch_iced aircraft_->Ch_iced
3036 #define fout aircraft_->fout
3038 bool ignore_unknown_keywords;
3039 #define ignore_unknown_keywords aircraft_->ignore_unknown_keywords
3042 #define ap_pah_on aircraft_->ap_pah_on
3043 double ap_pah_start_time;
3044 #define ap_pah_start_time aircraft_->ap_pah_start_time
3045 double ap_Theta_ref_rad;
3046 #define ap_Theta_ref_rad aircraft_->ap_Theta_ref_rad
3049 #define ap_alh_on aircraft_->ap_alh_on
3050 double ap_alh_start_time;
3051 #define ap_alh_start_time aircraft_->ap_alh_start_time
3052 double ap_alt_ref_ft;
3053 #define ap_alt_ref_ft aircraft_->ap_alt_ref_ft
3056 #define ap_rah_on aircraft_->ap_rah_on
3057 double ap_rah_start_time;
3058 #define ap_rah_start_time aircraft_->ap_rah_start_time
3059 double ap_Phi_ref_rad;
3060 #define ap_Phi_ref_rad aircraft_->ap_Phi_ref_rad
3063 #define ap_hh_on aircraft_->ap_hh_on
3064 double ap_hh_start_time;
3065 #define ap_hh_start_time aircraft_->ap_hh_start_time
3066 double ap_Psi_ref_rad;
3067 #define ap_Psi_ref_rad aircraft_->ap_Psi_ref_rad
3069 int pitch_trim_up, pitch_trim_down;
3070 #define pitch_trim_up aircraft_->pitch_trim_up
3071 #define pitch_trim_down aircraft_->pitch_trim_down
3073 bool pilot_throttle_no;
3074 #define pilot_throttle_no aircraft_->pilot_throttle_no
3076 int ice_tail, ice_left, ice_right;
3077 #define ice_tail aircraft_->ice_tail
3078 #define ice_left aircraft_->ice_left
3079 #define ice_right aircraft_->ice_right
3081 // Variables for the trigger command
3082 int trigger_on, trigger_last_time_step, trigger_num;
3083 int trigger_toggle, trigger_counter;
3084 #define trigger_on aircraft_->trigger_on
3085 #define trigger_last_time_step aircraft_->trigger_last_time_step
3086 #define trigger_num aircraft_->trigger_num
3087 #define trigger_toggle aircraft_->trigger_toggle
3088 #define trigger_counter aircraft_->trigger_counter
3090 // temp debug values
3091 double debug7, debug8, debug9, debug10;
3092 #define debug7 aircraft_->debug7
3093 #define debug8 aircraft_->debug8
3094 #define debug9 aircraft_->debug9
3095 #define debug10 aircraft_->debug10
3098 extern AIRCRAFT *aircraft_; // usually defined in the first program that includes uiuc_aircraft.h
3100 #endif // endif _AIRCRAFT_H