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
36 ----------------------------------------------------------------------
38 AUTHOR(S): Bipin Sehgal <bsehgal@uiuc.edu>
39 Jeff Scott <jscott@mail.com>
41 ----------------------------------------------------------------------
45 ----------------------------------------------------------------------
49 ----------------------------------------------------------------------
53 ----------------------------------------------------------------------
55 CALLED BY: uiuc_1DdataFileReader.cpp
56 uiuc_2DdataFileReader.cpp
57 uiuc_aerodeflections.cpp
60 uiuc_initializemaps.cpp
64 ----------------------------------------------------------------------
68 ----------------------------------------------------------------------
70 COPYRIGHT: (C) 2000 by Michael Selig
72 This program is free software; you can redistribute it and/or
73 modify it under the terms of the GNU General Public License
74 as published by the Free Software Foundation.
76 This program is distributed in the hope that it will be useful,
77 but WITHOUT ANY WARRANTY; without even the implied warranty of
78 MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
79 GNU General Public License for more details.
81 You should have received a copy of the GNU General Public License
82 along with this program; if not, write to the Free Software
83 Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307,
84 USA or view http://www.gnu.org/copyleft/gpl.html.
86 **********************************************************************/
94 #include "uiuc_parsefile.h"
96 typedef stack :: iterator LIST;
98 /* Add more keywords here if required*/
99 enum {init_flag = 1000, geometry_flag, controlSurface_flag, controlsMixer_flag,
100 mass_flag, engine_flag, CD_flag, CL_flag, Cm_flag, CY_flag, Cl_flag,
101 Cn_flag, gear_flag, ice_flag, record_flag};
103 // init ======= Initial values for equation of motion
104 enum {Dx_pilot_flag = 2000, Dy_pilot_flag, Dz_pilot_flag,
105 Dx_cg_flag, Dy_cg_flag, Dz_cg_flag,
106 V_north_flag, V_east_flag, V_down_flag,
107 P_body_flag, Q_body_flag, R_body_flag,
108 Phi_flag, Theta_flag, Psi_flag};
110 // geometry === Aircraft-specific geometric quantities
111 enum {bw_flag = 3000, cbar_flag, Sw_flag};
113 // controlSurface = Control surface deflections and properties
114 enum {de_flag = 4000, da_flag, dr_flag};
116 // controlsMixer == Controls mixer
117 enum {nomix_flag = 14000};
119 //mass ======== Aircraft-specific mass properties
120 enum {Mass_flag = 5000, I_xx_flag, I_yy_flag, I_zz_flag, I_xz_flag};
122 // engine ===== Propulsion data
123 enum {simpleSingle_flag = 6000, c172_flag};
125 // CD ========= Aerodynamic x-force quantities (longitudinal)
126 enum {CDo_flag = 7000, CDK_flag, CD_a_flag, CD_de_flag, CDfa_flag, CDfade_flag};
128 // CL ========= Aerodynamic z-force quantities (longitudinal)
129 enum {CLo_flag = 8000, CL_a_flag, CL_adot_flag, CL_q_flag, CL_de_flag, CLfa_flag, CLfade_flag};
131 // Cm ========= Aerodynamic m-moment quantities (longitudinal)
132 enum {Cmo_flag = 9000, Cm_a_flag, Cm_adot_flag, Cm_q_flag, Cm_de_flag, Cmfade_flag};
134 // CY ========= Aerodynamic y-force quantities (lateral)
135 enum {CYo_flag = 10000, CY_beta_flag, CY_p_flag, CY_r_flag, CY_da_flag, CY_dr_flag,
136 CYfada_flag, CYfbetadr_flag};
138 // Cl ========= Aerodynamic l-moment quantities (lateral)
139 enum {Clo_flag = 11000, Cl_beta_flag, Cl_betafCL_flag, Cl_p_flag, Cl_r_flag, Cl_rfCL_flag,
140 Cl_da_flag, Cl_dr_flag, Clfada_flag, Clfbetadr_flag};
142 // Cn ========= Aerodynamic n-moment quantities (lateral)
143 enum {Cno_flag = 12000, Cn_beta_flag, Cn_betafCL_flag, Cn_p_flag, Cn_pfCL_flag, Cn_r_flag,
144 Cn_rfCL_flag, Cn_da_flag, Cn_dr_flag, Cn_drfCL_flag, Cnfada_flag, Cnfbetadr_flag};
146 // gear ======= Landing gear model quantities
148 // ice ======== Ice model quantities
149 enum {iceTime_flag = 15000, transientTime_flag, eta_final_flag,
150 kCDo_flag, kCDK_flag, kCD_a_flag, kCD_de_flag,
151 kCLo_flag, kCL_a_flag, kCL_adot_flag, kCL_q_flag, kCL_de_flag,
152 kCmo_flag, kCm_a_flag, kCm_adot_flag, kCm_q_flag, kCm_de_flag,
153 kCYo_flag, kCY_beta_flag, kCY_p_flag, kCY_r_flag, kCY_da_flag, kCY_dr_flag,
154 kClo_flag, kCl_beta_flag, kCl_p_flag, kCl_r_flag, kCl_da_flag, kCl_dr_flag,
155 kCno_flag, kCn_beta_flag, kCn_p_flag, kCn_r_flag, kCn_da_flag, kCn_dr_flag};
157 // record ===== Record desired quantites to file
159 enum {Dx_pilot_record = 13000, Dy_pilot_record, Dz_pilot_record,
160 Dx_cg_record, Dy_cg_record, Dz_cg_record,
161 V_north_record, V_east_record, V_down_record,
162 V_rel_wind_record, Dynamic_pressure_record,
163 Alpha_record, Alpha_dot_record, Beta_record, Beta_dot_record, Gamma_record,
164 P_body_record, Q_body_record, R_body_record,
165 Phi_record, Theta_record, Psi_record, Theta_dot_record,
166 density_record, Mass_record, Simtime_record, dt_record,
167 elevator_record, aileron_record, rudder_record,
168 CD_record, CDfaI_record, CDfadeI_record,
169 CL_record, CLfaI_record, CLfadeI_record,
170 Cm_record, CmfadeI_record,
171 CY_record, CYfadaI_record, CYfbetadrI_record,
172 Cl_record, ClfadaI_record, ClfbetadrI_record,
173 Cn_record, CnfadaI_record, CnfbetadrI_record,
174 F_X_wind_record, F_Y_wind_record, F_Z_wind_record,
175 F_X_aero_record, F_Y_aero_record, F_Z_aero_record,
176 F_X_engine_record, F_Y_engine_record, F_Z_engine_record,
177 F_X_gear_record, F_Y_gear_record, F_Z_gear_record,
178 F_X_record, F_Y_record, F_Z_record,
179 M_l_aero_record, M_m_aero_record, M_n_aero_record,
180 M_l_engine_record, M_m_engine_record, M_n_engine_record,
181 M_l_gear_record, M_m_gear_record, M_n_gear_record,
182 M_l_rp_record, M_m_rp_record, M_n_rp_record};
186 // ParseFile stuff [] Bipin to add more comments
188 #define airplane aircraft_->airplane
189 ParseFile *initParts;
190 #define initParts aircraft_->initParts
191 ParseFile *geometryParts;
192 #define geometryParts aircraft_->geometryParts
193 ParseFile *massParts;
194 #define massParts aircraft_->massParts
195 ParseFile *aeroParts;
196 #define aeroParts aircraft_->aeroParts
197 ParseFile *engineParts;
198 #define engineParts aircraft_->engineParts
199 ParseFile *gearParts;
200 #define gearParts aircraft_->gearParts
201 ParseFile *recordParts;
202 #define recordParts aircraft_->recordParts
204 /*= Keywords (token1) ===========================================*/
205 map <string,int> Keyword_map;
206 #define Keyword_map aircraft_->Keyword_map
215 #define CL aircraft_->CL
216 #define CD aircraft_->CD
217 #define Cm aircraft_->Cm
218 #define CY aircraft_->CY
219 #define Cl aircraft_->Cl
220 #define Cn aircraft_->Cn
222 /*========================================*/
223 /* Variables (token2) - 14 groups (000210)*/
224 /*========================================*/
226 /* Variables (token2) ===========================================*/
227 /* init ========== Initial values for equations of motion =======*/
229 map <string,int> init_map;
230 #define init_map aircraft_->init_map
232 /* Variables (token2) ===========================================*/
233 /* geometry ====== Aircraft-specific geometric quantities =======*/
235 map <string,int> geometry_map;
236 #define geometry_map aircraft_->geometry_map
241 #define bw aircraft_->bw
242 #define cbar aircraft_->cbar
243 #define Sw aircraft_->Sw
245 /* Variables (token2) ===========================================*/
246 /* controlSurface Control surface deflections and properties ===*/
248 map <string,int> controlSurface_map;
249 #define controlSurface_map aircraft_->controlSurface_map
257 #define demax aircraft_->demax
258 #define demin aircraft_->demin
259 #define damax aircraft_->damax
260 #define damin aircraft_->damin
261 #define drmax aircraft_->drmax
262 #define drmin aircraft_->drmin
267 #define aileron aircraft_->aileron
268 #define elevator aircraft_->elevator
269 #define rudder aircraft_->rudder
272 /* Variables (token2) ===========================================*/
273 /* controlsMixer = Control mixer ================================*/
275 map <string,int> controlsMixer_map;
276 #define controlsMixer_map aircraft_->controlsMixer_map
279 #define nomix aircraft_->nomix
282 /* Variables (token2) ===========================================*/
283 /* mass =========== Aircraft-specific mass properties ===========*/
285 map <string,int> mass_map;
286 #define mass_map aircraft_->mass_map
289 /* Variables (token2) ===========================================*/
290 /* engine ======== Propulsion data ==============================*/
292 map <string,int> engine_map;
293 #define engine_map aircraft_->engine_map
295 double simpleSingleMaxThrust;
296 #define simpleSingleMaxThrust aircraft_->simpleSingleMaxThrust
298 /* Variables (token2) ===========================================*/
299 /* CD ============ Aerodynamic x-force quantities (longitudinal) */
301 map <string,int> CD_map;
302 #define CD_map aircraft_->CD_map
308 #define CDo aircraft_->CDo
309 #define CDK aircraft_->CDK
310 #define CD_a aircraft_->CD_a
311 #define CD_de aircraft_->CD_de
314 double CDfa_aArray[100];
315 double CDfa_CDArray[100];
318 #define CDfa aircraft_->CDfa
319 #define CDfaData aircraft_->CDfaData
320 #define CDfa_aArray aircraft_->CDfa_aArray
321 #define CDfa_CDArray aircraft_->CDfa_CDArray
322 #define CDfa_nAlpha aircraft_->CDfa_nAlpha
323 #define CDfaI aircraft_->CDfaI
326 double CDfade_aArray[100][100];
327 double CDfade_deArray[100];
328 double CDfade_CDArray[100][100];
329 int CDfade_nAlphaArray[100];
332 #define CDfade aircraft_->CDfade
333 #define CDfadeData aircraft_->CDfadeData
334 #define CDfade_aArray aircraft_->CDfade_aArray
335 #define CDfade_deArray aircraft_->CDfade_deArray
336 #define CDfade_CDArray aircraft_->CDfade_CDArray
337 #define CDfade_nAlphaArray aircraft_->CDfade_nAlphaArray
338 #define CDfade_nde aircraft_->CDfade_nde
339 #define CDfadeI aircraft_->CDfadeI
341 /* Variables (token2) ===========================================*/
342 /* CL ============ Aerodynamic z-force quantities (longitudinal) */
344 map <string,int> CL_map;
345 #define CL_map aircraft_->CL_map
352 #define CLo aircraft_->CLo
353 #define CL_a aircraft_->CL_a
354 #define CL_adot aircraft_->CL_adot
355 #define CL_q aircraft_->CL_q
356 #define CL_de aircraft_->CL_de
359 double CLfa_aArray[100];
360 double CLfa_CLArray[100];
363 #define CLfa aircraft_->CLfa
364 #define CLfaData aircraft_->CLfaData
365 #define CLfa_aArray aircraft_->CLfa_aArray
366 #define CLfa_CLArray aircraft_->CLfa_CLArray
367 #define CLfa_nAlpha aircraft_->CLfa_nAlpha
368 #define CLfaI aircraft_->CLfaI
371 double CLfade_aArray[100][100];
372 double CLfade_deArray[100];
373 double CLfade_CLArray[100][100];
374 int CLfade_nAlphaArray[100];
377 #define CLfade aircraft_->CLfade
378 #define CLfadeData aircraft_->CLfadeData
379 #define CLfade_aArray aircraft_->CLfade_aArray
380 #define CLfade_deArray aircraft_->CLfade_deArray
381 #define CLfade_CLArray aircraft_->CLfade_CLArray
382 #define CLfade_nAlphaArray aircraft_->CLfade_nAlphaArray
383 #define CLfade_nde aircraft_->CLfade_nde
384 #define CLfadeI aircraft_->CLfadeI
386 /* Variables (token2) ===========================================*/
387 /* Cm ============ Aerodynamic m-moment quantities (longitudinal) */
389 map <string,int> Cm_map;
390 #define Cm_map aircraft_->Cm_map
397 #define Cmo aircraft_->Cmo
398 #define Cm_a aircraft_->Cm_a
399 #define Cm_adot aircraft_->Cm_adot
400 #define Cm_q aircraft_->Cm_q
401 #define Cm_de aircraft_->Cm_de
404 double Cmfade_aArray[100][100];
405 double Cmfade_deArray[100];
406 double Cmfade_CmArray[100][100];
407 int Cmfade_nAlphaArray[100];
410 #define Cmfade aircraft_->Cmfade
411 #define CmfadeData aircraft_->CmfadeData
412 #define Cmfade_aArray aircraft_->Cmfade_aArray
413 #define Cmfade_deArray aircraft_->Cmfade_deArray
414 #define Cmfade_CmArray aircraft_->Cmfade_CmArray
415 #define Cmfade_nAlphaArray aircraft_->Cmfade_nAlphaArray
416 #define Cmfade_nde aircraft_->Cmfade_nde
417 #define CmfadeI aircraft_->CmfadeI
419 /* Variables (token2) ===========================================*/
420 /* CY ============ Aerodynamic y-force quantities (lateral) =====*/
422 map <string,int> CY_map;
423 #define CY_map aircraft_->CY_map
431 #define CYo aircraft_->CYo
432 #define CY_beta aircraft_->CY_beta
433 #define CY_p aircraft_->CY_p
434 #define CY_r aircraft_->CY_r
435 #define CY_da aircraft_->CY_da
436 #define CY_dr aircraft_->CY_dr
439 double CYfada_aArray[100][100];
440 double CYfada_daArray[100];
441 double CYfada_CYArray[100][100];
442 int CYfada_nAlphaArray[100];
445 #define CYfada aircraft_->CYfada
446 #define CYfadaData aircraft_->CYfadaData
447 #define CYfada_aArray aircraft_->CYfada_aArray
448 #define CYfada_daArray aircraft_->CYfada_daArray
449 #define CYfada_CYArray aircraft_->CYfada_CYArray
450 #define CYfada_nAlphaArray aircraft_->CYfada_nAlphaArray
451 #define CYfada_nda aircraft_->CYfada_nda
452 #define CYfadaI aircraft_->CYfadaI
455 double CYfbetadr_betaArray[100][100];
456 double CYfbetadr_drArray[100];
457 double CYfbetadr_CYArray[100][100];
458 int CYfbetadr_nBetaArray[100];
461 #define CYfbetadr aircraft_->CYfbetadr
462 #define CYfbetadrData aircraft_->CYfbetadrData
463 #define CYfbetadr_betaArray aircraft_->CYfbetadr_betaArray
464 #define CYfbetadr_drArray aircraft_->CYfbetadr_drArray
465 #define CYfbetadr_CYArray aircraft_->CYfbetadr_CYArray
466 #define CYfbetadr_nBetaArray aircraft_->CYfbetadr_nBetaArray
467 #define CYfbetadr_ndr aircraft_->CYfbetadr_ndr
468 #define CYfbetadrI aircraft_->CYfbetadrI
470 /* Variables (token2) ===========================================*/
471 /* Cl ============ Aerodynamic l-moment quantities (lateral) ====*/
473 map <string,int> Cl_map;
474 #define Cl_map aircraft_->Cl_map
484 #define Clo aircraft_->Clo
485 #define Cl_beta aircraft_->Cl_beta
486 #define Cl_betafCL aircraft_->Cl_betafCL
487 #define Cl_p aircraft_->Cl_p
488 #define Cl_r aircraft_->Cl_r
489 #define Cl_rfCL aircraft_->Cl_rfCL
490 #define Cl_da aircraft_->Cl_da
491 #define Cl_dr aircraft_->Cl_dr
494 double Clfada_aArray[100][100];
495 double Clfada_daArray[100];
496 double Clfada_ClArray[100][100];
497 int Clfada_nAlphaArray[100];
500 #define Clfada aircraft_->Clfada
501 #define ClfadaData aircraft_->ClfadaData
502 #define Clfada_aArray aircraft_->Clfada_aArray
503 #define Clfada_daArray aircraft_->Clfada_daArray
504 #define Clfada_ClArray aircraft_->Clfada_ClArray
505 #define Clfada_nAlphaArray aircraft_->Clfada_nAlphaArray
506 #define Clfada_nda aircraft_->Clfada_nda
507 #define ClfadaI aircraft_->ClfadaI
510 double Clfbetadr_betaArray[100][100];
511 double Clfbetadr_drArray[100];
512 double Clfbetadr_ClArray[100][100];
513 int Clfbetadr_nBetaArray[100];
516 #define Clfbetadr aircraft_->Clfbetadr
517 #define ClfbetadrData aircraft_->ClfbetadrData
518 #define Clfbetadr_betaArray aircraft_->Clfbetadr_betaArray
519 #define Clfbetadr_drArray aircraft_->Clfbetadr_drArray
520 #define Clfbetadr_ClArray aircraft_->Clfbetadr_ClArray
521 #define Clfbetadr_nBetaArray aircraft_->Clfbetadr_nBetaArray
522 #define Clfbetadr_ndr aircraft_->Clfbetadr_ndr
523 #define ClfbetadrI aircraft_->ClfbetadrI
525 /* Variables (token2) ===========================================*/
526 /* Cn ============ Aerodynamic n-moment quantities (lateral) ====*/
528 map <string,int> Cn_map;
529 #define Cn_map aircraft_->Cn_map
537 #define Cno aircraft_->Cno
538 #define Cn_beta aircraft_->Cn_beta
539 #define Cn_p aircraft_->Cn_p
540 #define Cn_r aircraft_->Cn_r
541 #define Cn_da aircraft_->Cn_da
542 #define Cn_dr aircraft_->Cn_dr
545 double Cnfada_aArray[100][100];
546 double Cnfada_daArray[100];
547 double Cnfada_CnArray[100][100];
548 int Cnfada_nAlphaArray[100];
551 #define Cnfada aircraft_->Cnfada
552 #define CnfadaData aircraft_->CnfadaData
553 #define Cnfada_aArray aircraft_->Cnfada_aArray
554 #define Cnfada_daArray aircraft_->Cnfada_daArray
555 #define Cnfada_CnArray aircraft_->Cnfada_CnArray
556 #define Cnfada_nAlphaArray aircraft_->Cnfada_nAlphaArray
557 #define Cnfada_nda aircraft_->Cnfada_nda
558 #define CnfadaI aircraft_->CnfadaI
561 double Cnfbetadr_betaArray[100][100];
562 double Cnfbetadr_drArray[100];
563 double Cnfbetadr_CnArray[100][100];
564 int Cnfbetadr_nBetaArray[100];
567 #define Cnfbetadr aircraft_->Cnfbetadr
568 #define CnfbetadrData aircraft_->CnfbetadrData
569 #define Cnfbetadr_betaArray aircraft_->Cnfbetadr_betaArray
570 #define Cnfbetadr_drArray aircraft_->Cnfbetadr_drArray
571 #define Cnfbetadr_CnArray aircraft_->Cnfbetadr_CnArray
572 #define Cnfbetadr_nBetaArray aircraft_->Cnfbetadr_nBetaArray
573 #define Cnfbetadr_ndr aircraft_->Cnfbetadr_ndr
574 #define CnfbetadrI aircraft_->CnfbetadrI
576 /* Variables (token2) ===========================================*/
577 /* gear ========== Landing gear model quantities ================*/
579 map <string,int> gear_map;
581 #define gear_map aircraft_->gear_map
583 /* Variables (token2) ===========================================*/
584 /* ice =========== Ice model quantities ======================== */
586 map <string,int> ice_map;
587 #define ice_map aircraft_->ice_map
590 double transientTime;
593 #define iceTime aircraft_->iceTime
594 #define transientTime aircraft_->transientTime
595 #define eta_final aircraft_->eta_final
596 #define eta aircraft_->eta
605 #define kCDo aircraft_->kCDo
606 #define kCDK aircraft_->kCDK
607 #define kCD_a aircraft_->kCD_a
608 #define kCD_de aircraft_->kCD_de
609 #define CDo_clean aircraft_->CDo_clean
610 #define CDK_clean aircraft_->CDK_clean
611 #define CD_a_clean aircraft_->CD_a_clean
612 #define CD_de_clean aircraft_->CD_de_clean
620 double CL_adot_clean;
623 #define kCLo aircraft_->kCLo
624 #define kCL_a aircraft_->kCL_a
625 #define kCL_adot aircraft_->kCL_adot
626 #define kCL_q aircraft_->kCL_q
627 #define kCL_de aircraft_->kCL_de
628 #define CLo_clean aircraft_->CLo_clean
629 #define CL_a_clean aircraft_->CL_a_clean
630 #define CL_adot_clean aircraft_->CL_adot_clean
631 #define CL_q_clean aircraft_->CL_q_clean
632 #define CL_de_clean aircraft_->CL_de_clean
640 double Cm_adot_clean;
643 #define kCmo aircraft_->kCmo
644 #define kCm_a aircraft_->kCm_a
645 #define kCm_adot aircraft_->kCm_adot
646 #define kCm_q aircraft_->kCm_q
647 #define kCm_de aircraft_->kCm_de
648 #define Cmo_clean aircraft_->Cmo_clean
649 #define Cm_a_clean aircraft_->Cm_a_clean
650 #define Cm_adot_clean aircraft_->Cm_adot_clean
651 #define Cm_q_clean aircraft_->Cm_q_clean
652 #define Cm_de_clean aircraft_->Cm_de_clean
660 double CY_beta_clean;
665 #define kCYo aircraft_->kCYo
666 #define kCY_beta aircraft_->kCY_beta
667 #define kCY_p aircraft_->kCY_p
668 #define kCY_r aircraft_->kCY_r
669 #define kCY_da aircraft_->kCY_da
670 #define kCY_dr aircraft_->kCY_dr
671 #define CYo_clean aircraft_->CYo_clean
672 #define CY_beta_clean aircraft_->CY_beta_clean
673 #define CY_p_clean aircraft_->CY_p_clean
674 #define CY_r_clean aircraft_->CY_r_clean
675 #define CY_da_clean aircraft_->CY_da_clean
676 #define CY_dr_clean aircraft_->CY_dr_clean
684 double Cl_beta_clean;
689 #define kClo aircraft_->kClo
690 #define kCl_beta aircraft_->kCl_beta
691 #define kCl_p aircraft_->kCl_p
692 #define kCl_r aircraft_->kCl_r
693 #define kCl_da aircraft_->kCl_da
694 #define kCl_dr aircraft_->kCl_dr
695 #define Clo_clean aircraft_->Clo_clean
696 #define Cl_beta_clean aircraft_->Cl_beta_clean
697 #define Cl_p_clean aircraft_->Cl_p_clean
698 #define Cl_r_clean aircraft_->Cl_r_clean
699 #define Cl_da_clean aircraft_->Cl_da_clean
700 #define Cl_dr_clean aircraft_->Cl_dr_clean
708 double Cn_beta_clean;
713 #define kCno aircraft_->kCno
714 #define kCn_beta aircraft_->kCn_beta
715 #define kCn_p aircraft_->kCn_p
716 #define kCn_r aircraft_->kCn_r
717 #define kCn_da aircraft_->kCn_da
718 #define kCn_dr aircraft_->kCn_dr
719 #define Cno_clean aircraft_->Cno_clean
720 #define Cn_beta_clean aircraft_->Cn_beta_clean
721 #define Cn_p_clean aircraft_->Cn_p_clean
722 #define Cn_r_clean aircraft_->Cn_r_clean
723 #define Cn_da_clean aircraft_->Cn_da_clean
724 #define Cn_dr_clean aircraft_->Cn_dr_clean
726 /* Variables (token2) ===========================================*/
727 /* record ======== Record desired quantites to file =============*/
729 map <string,int> record_map;
730 #define record_map aircraft_->record_map
732 /***** Forces *******/
734 double F_X_wind, F_Y_wind, F_Z_wind;
736 #define F_X_wind aircraft_->F_X_wind
737 #define F_Y_wind aircraft_->F_Y_wind
738 #define F_Z_wind aircraft_->F_Z_wind
741 /* Miscellaneous ================================================*/
743 int conversion1, conversion2, conversion3;
744 double confac1, confac2, confac3;
746 #define conversion1 aircraft_->conversion1
747 #define conversion2 aircraft_->conversion2
748 #define conversion3 aircraft_->conversion3
749 #define confac1 aircraft_->confac1
750 #define confac2 aircraft_->confac2
751 #define confac3 aircraft_->confac3
756 #define fout aircraft_->fout
761 // usually defined in the first program that includes uiuc_aircraft.h
762 extern AIRCRAFT *aircraft_;
764 #endif // endif _AIRCRAFT_H