1 /***************************************************************************
5 ----------------------------------------------------------------------------
7 FUNCTION: LaRCSim generic parameters header file
9 ----------------------------------------------------------------------------
11 MODULE STATUS: developmental
13 ----------------------------------------------------------------------------
15 GENEALOGY: Created 15 DEC 1993 by Bruce Jackson;
16 was part of old ls_eom.h header
18 ----------------------------------------------------------------------------
20 DESIGNED BY: B. Jackson
24 MAINTAINED BY: guess who
26 ----------------------------------------------------------------------------
33 ----------------------------------------------------------------------------
37 [ 1] McFarland, Richard E.: "A Standard Kinematic Model
38 for Flight Simulation at NASA-Ames", NASA CR-2497,
41 [ 2] ANSI/AIAA R-004-1992 "Recommended Practice: Atmos-
42 pheric and Space Flight Vehicle Coordinate Systems",
45 [ 3] Beyer, William H., editor: "CRC Standard Mathematical
46 Tables, 28th edition", CRC Press, Boca Raton, FL, 1987,
49 [ 4] Dowdy, M. C.; Jackson, E. B.; and Nichols, J. H.:
50 "Controls Analysis and Simulation Test Loop Environ-
51 ment (CASTLE) Programmer's Guide, Version 1.3",
52 NATC TM 89-11, 30 March 1989.
54 [ 5] Halliday, David; and Resnick, Robert: "Fundamentals
55 of Physics, Revised Printing", Wiley and Sons, 1974.
58 [ 6] Anon: "U. S. Standard Atmosphere, 1962"
60 [ 7] Anon: "Aeronautical Vest Pocket Handbook, 17th edition",
61 Pratt & Whitney Aircraft Group, Dec. 1977
63 [ 8] Stevens, Brian L.; and Lewis, Frank L.: "Aircraft
64 Control and Simulation", Wiley and Sons, 1992.
67 --------------------------------------------------------------------------*/
85 * Needed for windows builds
91 /*================== Mass properties and geometry values ==================*/
93 DATA mass, i_xx, i_yy, i_zz, i_xz; /* Inertias */
94 #define Mass generic_.mass
95 #define I_xx generic_.i_xx
96 #define I_yy generic_.i_yy
97 #define I_zz generic_.i_zz
98 #define I_xz generic_.i_xz
100 VECTOR_3 d_pilot_rp_body_v; /* Pilot location rel to ref pt */
101 #define D_pilot_rp_body_v generic_.d_pilot_rp_body_v
102 #define Dx_pilot generic_.d_pilot_rp_body_v[0]
103 #define Dy_pilot generic_.d_pilot_rp_body_v[1]
104 #define Dz_pilot generic_.d_pilot_rp_body_v[2]
106 VECTOR_3 d_cg_rp_body_v; /* CG position w.r.t. ref. point */
107 #define D_cg_rp_body_v generic_.d_cg_rp_body_v
108 #define Dx_cg generic_.d_cg_rp_body_v[0]
109 #define Dy_cg generic_.d_cg_rp_body_v[1]
110 #define Dz_cg generic_.d_cg_rp_body_v[2]
112 /*================================ Forces =================================*/
114 VECTOR_3 f_body_total_v;
115 #define F_body_total_v generic_.f_body_total_v
116 #define F_X generic_.f_body_total_v[0]
117 #define F_Y generic_.f_body_total_v[1]
118 #define F_Z generic_.f_body_total_v[2]
120 VECTOR_3 f_local_total_v;
121 #define F_local_total_v generic_.f_local_total_v
122 #define F_north generic_.f_local_total_v[0]
123 #define F_east generic_.f_local_total_v[1]
124 #define F_down generic_.f_local_total_v[2]
127 #define F_aero_v generic_.f_aero_v
128 #define F_X_aero generic_.f_aero_v[0]
129 #define F_Y_aero generic_.f_aero_v[1]
130 #define F_Z_aero generic_.f_aero_v[2]
133 #define F_engine_v generic_.f_engine_v
134 #define F_X_engine generic_.f_engine_v[0]
135 #define F_Y_engine generic_.f_engine_v[1]
136 #define F_Z_engine generic_.f_engine_v[2]
138 int use_external_engine;
139 #define Use_External_Engine generic_.use_external_engine
142 #define F_gear_v generic_.f_gear_v
143 #define F_X_gear generic_.f_gear_v[0]
144 #define F_Y_gear generic_.f_gear_v[1]
145 #define F_Z_gear generic_.f_gear_v[2]
147 /*================================ Moments ================================*/
149 VECTOR_3 m_total_rp_v;
150 #define M_total_rp_v generic_.m_total_rp_v
151 #define M_l_rp generic_.m_total_rp_v[0]
152 #define M_m_rp generic_.m_total_rp_v[1]
153 #define M_n_rp generic_.m_total_rp_v[2]
155 VECTOR_3 m_total_cg_v;
156 #define M_total_cg_v generic_.m_total_cg_v
157 #define M_l_cg generic_.m_total_cg_v[0]
158 #define M_m_cg generic_.m_total_cg_v[1]
159 #define M_n_cg generic_.m_total_cg_v[2]
162 #define M_aero_v generic_.m_aero_v
163 #define M_l_aero generic_.m_aero_v[0]
164 #define M_m_aero generic_.m_aero_v[1]
165 #define M_n_aero generic_.m_aero_v[2]
168 #define M_engine_v generic_.m_engine_v
169 #define M_l_engine generic_.m_engine_v[0]
170 #define M_m_engine generic_.m_engine_v[1]
171 #define M_n_engine generic_.m_engine_v[2]
174 #define M_gear_v generic_.m_gear_v
175 #define M_l_gear generic_.m_gear_v[0]
176 #define M_m_gear generic_.m_gear_v[1]
177 #define M_n_gear generic_.m_gear_v[2]
179 /*============================== Accelerations ============================*/
181 VECTOR_3 v_dot_local_v;
182 #define V_dot_local_v generic_.v_dot_local_v
183 #define V_dot_north generic_.v_dot_local_v[0]
184 #define V_dot_east generic_.v_dot_local_v[1]
185 #define V_dot_down generic_.v_dot_local_v[2]
187 VECTOR_3 v_dot_body_v;
188 #define V_dot_body_v generic_.v_dot_body_v
189 #define U_dot_body generic_.v_dot_body_v[0]
190 #define V_dot_body generic_.v_dot_body_v[1]
191 #define W_dot_body generic_.v_dot_body_v[2]
193 VECTOR_3 a_cg_body_v;
194 #define A_cg_body_v generic_.a_cg_body_v
195 #define A_X_cg generic_.a_cg_body_v[0]
196 #define A_Y_cg generic_.a_cg_body_v[1]
197 #define A_Z_cg generic_.a_cg_body_v[2]
199 VECTOR_3 a_pilot_body_v;
200 #define A_pilot_body_v generic_.a_pilot_body_v
201 #define A_X_pilot generic_.a_pilot_body_v[0]
202 #define A_Y_pilot generic_.a_pilot_body_v[1]
203 #define A_Z_pilot generic_.a_pilot_body_v[2]
205 VECTOR_3 n_cg_body_v;
206 #define N_cg_body_v generic_.n_cg_body_v
207 #define N_X_cg generic_.n_cg_body_v[0]
208 #define N_Y_cg generic_.n_cg_body_v[1]
209 #define N_Z_cg generic_.n_cg_body_v[2]
211 VECTOR_3 n_pilot_body_v;
212 #define N_pilot_body_v generic_.n_pilot_body_v
213 #define N_X_pilot generic_.n_pilot_body_v[0]
214 #define N_Y_pilot generic_.n_pilot_body_v[1]
215 #define N_Z_pilot generic_.n_pilot_body_v[2]
217 VECTOR_3 omega_dot_body_v;
218 #define Omega_dot_body_v generic_.omega_dot_body_v
219 #define P_dot_body generic_.omega_dot_body_v[0]
220 #define Q_dot_body generic_.omega_dot_body_v[1]
221 #define R_dot_body generic_.omega_dot_body_v[2]
224 /*============================== Velocities ===============================*/
227 #define V_local_v generic_.v_local_v
228 #define V_north generic_.v_local_v[0]
229 #define V_east generic_.v_local_v[1]
230 #define V_down generic_.v_local_v[2]
232 VECTOR_3 v_local_rel_ground_v; /* V rel w.r.t. earth surface */
233 #define V_local_rel_ground_v generic_.v_local_rel_ground_v
234 #define V_north_rel_ground generic_.v_local_rel_ground_v[0]
235 #define V_east_rel_ground generic_.v_local_rel_ground_v[1]
236 #define V_down_rel_ground generic_.v_local_rel_ground_v[2]
238 VECTOR_3 v_local_airmass_v; /* velocity of airmass (steady winds) */
239 #define V_local_airmass_v generic_.v_local_airmass_v
240 #define V_north_airmass generic_.v_local_airmass_v[0]
241 #define V_east_airmass generic_.v_local_airmass_v[1]
242 #define V_down_airmass generic_.v_local_airmass_v[2]
244 VECTOR_3 v_local_rel_airmass_v; /* velocity of veh. relative to airmass */
245 #define V_local_rel_airmass_v generic_.v_local_rel_airmass_v
246 #define V_north_rel_airmass generic_.v_local_rel_airmass_v[0]
247 #define V_east_rel_airmass generic_.v_local_rel_airmass_v[1]
248 #define V_down_rel_airmass generic_.v_local_rel_airmass_v[2]
250 VECTOR_3 v_local_gust_v; /* linear turbulence components, L frame */
251 #define V_local_gust_v generic_.v_local_gust_v
252 #define U_gust generic_.v_local_gust_v[0]
253 #define V_gust generic_.v_local_gust_v[1]
254 #define W_gust generic_.v_local_gust_v[2]
256 VECTOR_3 v_wind_body_v; /* Wind-relative velocities in body axis */
257 #define V_wind_body_v generic_.v_wind_body_v
258 #define U_body generic_.v_wind_body_v[0]
259 #define V_body generic_.v_wind_body_v[1]
260 #define W_body generic_.v_wind_body_v[2]
262 DATA v_rel_wind, v_true_kts, v_rel_ground, v_inertial;
263 DATA v_ground_speed, v_equiv, v_equiv_kts;
264 DATA v_calibrated, v_calibrated_kts;
265 #define V_rel_wind generic_.v_rel_wind
266 #define V_true_kts generic_.v_true_kts
267 #define V_rel_ground generic_.v_rel_ground
268 #define V_inertial generic_.v_inertial
269 #define V_ground_speed generic_.v_ground_speed
270 #define V_equiv generic_.v_equiv
271 #define V_equiv_kts generic_.v_equiv_kts
272 #define V_calibrated generic_.v_calibrated
273 #define V_calibrated_kts generic_.v_calibrated_kts
275 VECTOR_3 omega_body_v; /* Angular B rates */
276 #define Omega_body_v generic_.omega_body_v
277 #define P_body generic_.omega_body_v[0]
278 #define Q_body generic_.omega_body_v[1]
279 #define R_body generic_.omega_body_v[2]
281 VECTOR_3 omega_local_v; /* Angular L rates */
282 #define Omega_local_v generic_.omega_local_v
283 #define P_local generic_.omega_local_v[0]
284 #define Q_local generic_.omega_local_v[1]
285 #define R_local generic_.omega_local_v[2]
287 VECTOR_3 omega_total_v; /* Diff btw B & L */
288 #define Omega_total_v generic_.omega_total_v
289 #define P_total generic_.omega_total_v[0]
290 #define Q_total generic_.omega_total_v[1]
291 #define R_total generic_.omega_total_v[2]
293 VECTOR_3 euler_rates_v;
294 #define Euler_rates_v generic_.euler_rates_v
295 #define Phi_dot generic_.euler_rates_v[0]
296 #define Theta_dot generic_.euler_rates_v[1]
297 #define Psi_dot generic_.euler_rates_v[2]
299 VECTOR_3 geocentric_rates_v; /* Geocentric linear velocities */
300 #define Geocentric_rates_v generic_.geocentric_rates_v
301 #define Latitude_dot generic_.geocentric_rates_v[0]
302 #define Longitude_dot generic_.geocentric_rates_v[1]
303 #define Radius_dot generic_.geocentric_rates_v[2]
305 /*=============================== Positions ===============================*/
307 VECTOR_3 geocentric_position_v;
308 #define Geocentric_position_v generic_.geocentric_position_v
309 #define Lat_geocentric generic_.geocentric_position_v[0]
310 #define Lon_geocentric generic_.geocentric_position_v[1]
311 #define Radius_to_vehicle generic_.geocentric_position_v[2]
313 VECTOR_3 geodetic_position_v;
314 #define Geodetic_position_v generic_.geodetic_position_v
315 #define Latitude generic_.geodetic_position_v[0]
316 #define Longitude generic_.geodetic_position_v[1]
317 #define Altitude generic_.geodetic_position_v[2]
319 VECTOR_3 euler_angles_v;
320 #define Euler_angles_v generic_.euler_angles_v
321 #define Phi generic_.euler_angles_v[0]
322 #define Theta generic_.euler_angles_v[1]
323 #define Psi generic_.euler_angles_v[2]
325 /*======================= Miscellaneous quantities ========================*/
327 DATA t_local_to_body_m[3][3]; /* Transformation matrix L to B */
328 #define T_local_to_body_m generic_.t_local_to_body_m
329 #define T_local_to_body_11 generic_.t_local_to_body_m[0][0]
330 #define T_local_to_body_12 generic_.t_local_to_body_m[0][1]
331 #define T_local_to_body_13 generic_.t_local_to_body_m[0][2]
332 #define T_local_to_body_21 generic_.t_local_to_body_m[1][0]
333 #define T_local_to_body_22 generic_.t_local_to_body_m[1][1]
334 #define T_local_to_body_23 generic_.t_local_to_body_m[1][2]
335 #define T_local_to_body_31 generic_.t_local_to_body_m[2][0]
336 #define T_local_to_body_32 generic_.t_local_to_body_m[2][1]
337 #define T_local_to_body_33 generic_.t_local_to_body_m[2][2]
339 DATA gravity; /* Local acceleration due to G */
340 #define Gravity generic_.gravity
342 DATA centrifugal_relief; /* load factor reduction due to speed */
343 #define Centrifugal_relief generic_.centrifugal_relief
345 DATA alpha, beta, alpha_dot, beta_dot; /* in radians */
346 #define Alpha generic_.alpha
347 #define Beta generic_.beta
348 #define Alpha_dot generic_.alpha_dot
349 #define Beta_dot generic_.beta_dot
351 DATA cos_alpha, sin_alpha, cos_beta, sin_beta;
352 #define Cos_alpha generic_.cos_alpha
353 #define Sin_alpha generic_.sin_alpha
354 #define Cos_beta generic_.cos_beta
355 #define Sin_beta generic_.sin_beta
357 DATA cos_phi, sin_phi, cos_theta, sin_theta, cos_psi, sin_psi;
358 #define Cos_phi generic_.cos_phi
359 #define Sin_phi generic_.sin_phi
360 #define Cos_theta generic_.cos_theta
361 #define Sin_theta generic_.sin_theta
362 #define Cos_psi generic_.cos_psi
363 #define Sin_psi generic_.sin_psi
365 DATA gamma_vert_rad, gamma_horiz_rad; /* Flight path angles */
366 #define Gamma_vert_rad generic_.gamma_vert_rad
367 #define Gamma_horiz_rad generic_.gamma_horiz_rad
369 DATA sigma, density, v_sound, mach_number;
370 #define Sigma generic_.sigma
371 #define Density generic_.density
372 #define V_sound generic_.v_sound
373 #define Mach_number generic_.mach_number
375 DATA static_pressure, total_pressure, impact_pressure, dynamic_pressure;
376 #define Static_pressure generic_.static_pressure
377 #define Total_pressure generic_.total_pressure
378 #define Impact_pressure generic_.impact_pressure
379 #define Dynamic_pressure generic_.dynamic_pressure
381 DATA static_temperature, total_temperature;
382 #define Static_temperature generic_.static_temperature
383 #define Total_temperature generic_.total_temperature
385 DATA sea_level_radius, earth_position_angle;
386 #define Sea_level_radius generic_.sea_level_radius
387 #define Earth_position_angle generic_.earth_position_angle
389 DATA runway_altitude, runway_latitude, runway_longitude, runway_heading;
390 #define Runway_altitude generic_.runway_altitude
391 #define Runway_latitude generic_.runway_latitude
392 #define Runway_longitude generic_.runway_longitude
393 #define Runway_heading generic_.runway_heading
396 #define Radius_to_rwy generic_.radius_to_rwy
398 VECTOR_3 d_cg_rwy_local_v; /* CG rel. to rwy in local coords */
399 #define D_cg_rwy_local_v generic_.d_cg_rwy_local_v
400 #define D_cg_north_of_rwy generic_.d_cg_rwy_local_v[0]
401 #define D_cg_east_of_rwy generic_.d_cg_rwy_local_v[1]
402 #define D_cg_above_rwy generic_.d_cg_rwy_local_v[2]
404 VECTOR_3 d_cg_rwy_rwy_v; /* CG relative to runway, in rwy coordinates */
405 #define D_cg_rwy_rwy_v generic_.d_cg_rwy_rwy_v
406 #define X_cg_rwy generic_.d_cg_rwy_rwy_v[0]
407 #define Y_cg_rwy generic_.d_cg_rwy_rwy_v[1]
408 #define H_cg_rwy generic_.d_cg_rwy_rwy_v[2]
410 VECTOR_3 d_pilot_rwy_local_v; /* pilot rel. to rwy in local coords */
411 #define D_pilot_rwy_local_v generic_.d_pilot_rwy_local_v
412 #define D_pilot_north_of_rwy generic_.d_pilot_rwy_local_v[0]
413 #define D_pilot_east_of_rwy generic_.d_pilot_rwy_local_v[1]
414 #define D_pilot_above_rwy generic_.d_pilot_rwy_local_v[2]
416 VECTOR_3 d_pilot_rwy_rwy_v; /* pilot rel. to rwy, in rwy coords. */
417 #define D_pilot_rwy_rwy_v generic_.d_pilot_rwy_rwy_v
418 #define X_pilot_rwy generic_.d_pilot_rwy_rwy_v[0]
419 #define Y_pilot_rwy generic_.d_pilot_rwy_rwy_v[1]
420 #define H_pilot_rwy generic_.d_pilot_rwy_rwy_v[2]
425 extern GENERIC generic_; /* usually defined in ls_main.c */
433 #endif /* _LS_GENERIC_H */
436 /*--------------------------- end of ls_generic.h ------------------------*/