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 --------------------------------------------------------------------------*/
71 /*================== Mass properties and geometry values ==================*/
73 DATA mass, i_xx, i_yy, i_zz, i_xz; /* Inertias */
74 #define Mass generic_.mass
75 #define I_xx generic_.i_xx
76 #define I_yy generic_.i_yy
77 #define I_zz generic_.i_zz
78 #define I_xz generic_.i_xz
80 VECTOR_3 d_pilot_rp_body_v; /* Pilot location rel to ref pt */
81 #define D_pilot_rp_body_v generic_.d_pilot_rp_body_v
82 #define Dx_pilot generic_.d_pilot_rp_body_v[0]
83 #define Dy_pilot generic_.d_pilot_rp_body_v[1]
84 #define Dz_pilot generic_.d_pilot_rp_body_v[2]
86 VECTOR_3 d_cg_rp_body_v; /* CG position w.r.t. ref. point */
87 #define D_cg_rp_body_v generic_.d_cg_rp_body_v
88 #define Dx_cg generic_.d_cg_rp_body_v[0]
89 #define Dy_cg generic_.d_cg_rp_body_v[1]
90 #define Dz_cg generic_.d_cg_rp_body_v[2]
92 /*================================ Forces =================================*/
94 VECTOR_3 f_body_total_v;
95 #define F_body_total_v generic_.f_body_total_v
96 #define F_X generic_.f_body_total_v[0]
97 #define F_Y generic_.f_body_total_v[1]
98 #define F_Z generic_.f_body_total_v[2]
100 VECTOR_3 f_local_total_v;
101 #define F_local_total_v generic_.f_local_total_v
102 #define F_north generic_.f_local_total_v[0]
103 #define F_east generic_.f_local_total_v[1]
104 #define F_down generic_.f_local_total_v[2]
107 #define F_aero_v generic_.f_aero_v
108 #define F_X_aero generic_.f_aero_v[0]
109 #define F_Y_aero generic_.f_aero_v[1]
110 #define F_Z_aero generic_.f_aero_v[2]
113 #define F_engine_v generic_.f_engine_v
114 #define F_X_engine generic_.f_engine_v[0]
115 #define F_Y_engine generic_.f_engine_v[1]
116 #define F_Z_engine generic_.f_engine_v[2]
119 #define F_gear_v generic_.f_gear_v
120 #define F_X_gear generic_.f_gear_v[0]
121 #define F_Y_gear generic_.f_gear_v[1]
122 #define F_Z_gear generic_.f_gear_v[2]
124 /*================================ Moments ================================*/
126 VECTOR_3 m_total_rp_v;
127 #define M_total_rp_v generic_.m_total_rp_v
128 #define M_l_rp generic_.m_total_rp_v[0]
129 #define M_m_rp generic_.m_total_rp_v[1]
130 #define M_n_rp generic_.m_total_rp_v[2]
132 VECTOR_3 m_total_cg_v;
133 #define M_total_cg_v generic_.m_total_cg_v
134 #define M_l_cg generic_.m_total_cg_v[0]
135 #define M_m_cg generic_.m_total_cg_v[1]
136 #define M_n_cg generic_.m_total_cg_v[2]
139 #define M_aero_v generic_.m_aero_v
140 #define M_l_aero generic_.m_aero_v[0]
141 #define M_m_aero generic_.m_aero_v[1]
142 #define M_n_aero generic_.m_aero_v[2]
145 #define M_engine_v generic_.m_engine_v
146 #define M_l_engine generic_.m_engine_v[0]
147 #define M_m_engine generic_.m_engine_v[1]
148 #define M_n_engine generic_.m_engine_v[2]
151 #define M_gear_v generic_.m_gear_v
152 #define M_l_gear generic_.m_gear_v[0]
153 #define M_m_gear generic_.m_gear_v[1]
154 #define M_n_gear generic_.m_gear_v[2]
156 /*============================== Accelerations ============================*/
158 VECTOR_3 v_dot_local_v;
159 #define V_dot_local_v generic_.v_dot_local_v
160 #define V_dot_north generic_.v_dot_local_v[0]
161 #define V_dot_east generic_.v_dot_local_v[1]
162 #define V_dot_down generic_.v_dot_local_v[2]
164 VECTOR_3 v_dot_body_v;
165 #define V_dot_body_v generic_.v_dot_body_v
166 #define U_dot_body generic_.v_dot_body_v[0]
167 #define V_dot_body generic_.v_dot_body_v[1]
168 #define W_dot_body generic_.v_dot_body_v[2]
170 VECTOR_3 a_cg_body_v;
171 #define A_cg_body_v generic_.a_cg_body_v
172 #define A_X_cg generic_.a_cg_body_v[0]
173 #define A_Y_cg generic_.a_cg_body_v[1]
174 #define A_Z_cg generic_.a_cg_body_v[2]
176 VECTOR_3 a_pilot_body_v;
177 #define A_pilot_body_v generic_.a_pilot_body_v
178 #define A_X_pilot generic_.a_pilot_body_v[0]
179 #define A_Y_pilot generic_.a_pilot_body_v[1]
180 #define A_Z_pilot generic_.a_pilot_body_v[2]
182 VECTOR_3 n_cg_body_v;
183 #define N_cg_body_v generic_.n_cg_body_v
184 #define N_X_cg generic_.n_cg_body_v[0]
185 #define N_Y_cg generic_.n_cg_body_v[1]
186 #define N_Z_cg generic_.n_cg_body_v[2]
188 VECTOR_3 n_pilot_body_v;
189 #define N_pilot_body_v generic_.n_pilot_body_v
190 #define N_X_pilot generic_.n_pilot_body_v[0]
191 #define N_Y_pilot generic_.n_pilot_body_v[1]
192 #define N_Z_pilot generic_.n_pilot_body_v[2]
194 VECTOR_3 omega_dot_body_v;
195 #define Omega_dot_body_v generic_.omega_dot_body_v
196 #define P_dot_body generic_.omega_dot_body_v[0]
197 #define Q_dot_body generic_.omega_dot_body_v[1]
198 #define R_dot_body generic_.omega_dot_body_v[2]
201 /*============================== Velocities ===============================*/
204 #define V_local_v generic_.v_local_v
205 #define V_north generic_.v_local_v[0]
206 #define V_east generic_.v_local_v[1]
207 #define V_down generic_.v_local_v[2]
209 VECTOR_3 v_local_rel_ground_v; /* V rel w.r.t. earth surface */
210 #define V_local_rel_ground_v generic_.v_local_rel_ground_v
211 #define V_north_rel_ground generic_.v_local_rel_ground_v[0]
212 #define V_east_rel_ground generic_.v_local_rel_ground_v[1]
213 #define V_down_rel_ground generic_.v_local_rel_ground_v[2]
215 VECTOR_3 v_local_airmass_v; /* velocity of airmass (steady winds) */
216 #define V_local_airmass_v generic_.v_local_airmass_v
217 #define V_north_airmass generic_.v_local_airmass_v[0]
218 #define V_east_airmass generic_.v_local_airmass_v[1]
219 #define V_down_airmass generic_.v_local_airmass_v[2]
221 VECTOR_3 v_local_rel_airmass_v; /* velocity of veh. relative to airmass */
222 #define V_local_rel_airmass_v generic_.v_local_rel_airmass_v
223 #define V_north_rel_airmass generic_.v_local_rel_airmass_v[0]
224 #define V_east_rel_airmass generic_.v_local_rel_airmass_v[1]
225 #define V_down_rel_airmass generic_.v_local_rel_airmass_v[2]
227 VECTOR_3 v_local_gust_v; /* linear turbulence components, L frame */
228 #define V_local_gust_v generic_.v_local_gust_v
229 #define U_gust generic_.v_local_gust_v[0]
230 #define V_gust generic_.v_local_gust_v[1]
231 #define W_gust generic_.v_local_gust_v[2]
233 VECTOR_3 v_wind_body_v; /* Wind-relative velocities in body axis */
234 #define V_wind_body_v generic_.v_wind_body_v
235 #define U_body generic_.v_wind_body_v[0]
236 #define V_body generic_.v_wind_body_v[1]
237 #define W_body generic_.v_wind_body_v[2]
239 DATA v_rel_wind, v_true_kts, v_rel_ground, v_inertial;
240 DATA v_ground_speed, v_equiv, v_equiv_kts;
241 DATA v_calibrated, v_calibrated_kts;
242 #define V_rel_wind generic_.v_rel_wind
243 #define V_true_kts generic_.v_true_kts
244 #define V_rel_ground generic_.v_rel_ground
245 #define V_inertial generic_.v_inertial
246 #define V_ground_speed generic_.v_ground_speed
247 #define V_equiv generic_.v_equiv
248 #define V_equiv_kts generic_.v_equiv_kts
249 #define V_calibrated generic_.v_calibrated
250 #define V_calibrated_kts generic_.v_calibrated_kts
252 VECTOR_3 omega_body_v; /* Angular B rates */
253 #define Omega_body_v generic_.omega_body_v
254 #define P_body generic_.omega_body_v[0]
255 #define Q_body generic_.omega_body_v[1]
256 #define R_body generic_.omega_body_v[2]
258 VECTOR_3 omega_local_v; /* Angular L rates */
259 #define Omega_local_v generic_.omega_local_v
260 #define P_local generic_.omega_local_v[0]
261 #define Q_local generic_.omega_local_v[1]
262 #define R_local generic_.omega_local_v[2]
264 VECTOR_3 omega_total_v; /* Diff btw B & L */
265 #define Omega_total_v generic_.omega_total_v
266 #define P_total generic_.omega_total_v[0]
267 #define Q_total generic_.omega_total_v[1]
268 #define R_total generic_.omega_total_v[2]
270 VECTOR_3 euler_rates_v;
271 #define Euler_rates_v generic_.euler_rates_v
272 #define Phi_dot generic_.euler_rates_v[0]
273 #define Theta_dot generic_.euler_rates_v[1]
274 #define Psi_dot generic_.euler_rates_v[2]
276 VECTOR_3 geocentric_rates_v; /* Geocentric linear velocities */
277 #define Geocentric_rates_v generic_.geocentric_rates_v
278 #define Latitude_dot generic_.geocentric_rates_v[0]
279 #define Longitude_dot generic_.geocentric_rates_v[1]
280 #define Radius_dot generic_.geocentric_rates_v[2]
282 /*=============================== Positions ===============================*/
284 VECTOR_3 geocentric_position_v;
285 #define Geocentric_position_v generic_.geocentric_position_v
286 #define Lat_geocentric generic_.geocentric_position_v[0]
287 #define Lon_geocentric generic_.geocentric_position_v[1]
288 #define Radius_to_vehicle generic_.geocentric_position_v[2]
290 VECTOR_3 geodetic_position_v;
291 #define Geodetic_position_v generic_.geodetic_position_v
292 #define Latitude generic_.geodetic_position_v[0]
293 #define Longitude generic_.geodetic_position_v[1]
294 #define Altitude generic_.geodetic_position_v[2]
296 VECTOR_3 euler_angles_v;
297 #define Euler_angles_v generic_.euler_angles_v
298 #define Phi generic_.euler_angles_v[0]
299 #define Theta generic_.euler_angles_v[1]
300 #define Psi generic_.euler_angles_v[2]
302 /*======================= Miscellaneous quantities ========================*/
304 DATA t_local_to_body_m[3][3]; /* Transformation matrix L to B */
305 #define T_local_to_body_m generic_.t_local_to_body_m
306 #define T_local_to_body_11 generic_.t_local_to_body_m[0][0]
307 #define T_local_to_body_12 generic_.t_local_to_body_m[0][1]
308 #define T_local_to_body_13 generic_.t_local_to_body_m[0][2]
309 #define T_local_to_body_21 generic_.t_local_to_body_m[1][0]
310 #define T_local_to_body_22 generic_.t_local_to_body_m[1][1]
311 #define T_local_to_body_23 generic_.t_local_to_body_m[1][2]
312 #define T_local_to_body_31 generic_.t_local_to_body_m[2][0]
313 #define T_local_to_body_32 generic_.t_local_to_body_m[2][1]
314 #define T_local_to_body_33 generic_.t_local_to_body_m[2][2]
316 DATA gravity; /* Local acceleration due to G */
317 #define Gravity generic_.gravity
319 DATA centrifugal_relief; /* load factor reduction due to speed */
320 #define Centrifugal_relief generic_.centrifugal_relief
322 DATA alpha, beta, alpha_dot, beta_dot; /* in radians */
323 #define Alpha generic_.alpha
324 #define Beta generic_.beta
325 #define Alpha_dot generic_.alpha_dot
326 #define Beta_dot generic_.beta_dot
328 DATA cos_alpha, sin_alpha, cos_beta, sin_beta;
329 #define Cos_alpha generic_.cos_alpha
330 #define Sin_alpha generic_.sin_alpha
331 #define Cos_beta generic_.cos_beta
332 #define Sin_beta generic_.sin_beta
334 DATA cos_phi, sin_phi, cos_theta, sin_theta, cos_psi, sin_psi;
335 #define Cos_phi generic_.cos_phi
336 #define Sin_phi generic_.sin_phi
337 #define Cos_theta generic_.cos_theta
338 #define Sin_theta generic_.sin_theta
339 #define Cos_psi generic_.cos_psi
340 #define Sin_psi generic_.sin_psi
342 DATA gamma_vert_rad, gamma_horiz_rad; /* Flight path angles */
343 #define Gamma_vert_rad generic_.gamma_vert_rad
344 #define Gamma_horiz_rad generic_.gamma_horiz_rad
346 DATA sigma, density, v_sound, mach_number;
347 #define Sigma generic_.sigma
348 #define Density generic_.density
349 #define V_sound generic_.v_sound
350 #define Mach_number generic_.mach_number
352 DATA static_pressure, total_pressure, impact_pressure, dynamic_pressure;
353 #define Static_pressure generic_.static_pressure
354 #define Total_pressure generic_.total_pressure
355 #define Impact_pressure generic_.impact_pressure
356 #define Dynamic_pressure generic_.dynamic_pressure
358 DATA static_temperature, total_temperature;
359 #define Static_temperature generic_.static_temperature
360 #define Total_temperature generic_.total_temperature
362 DATA sea_level_radius, earth_position_angle;
363 #define Sea_level_radius generic_.sea_level_radius
364 #define Earth_position_angle generic_.earth_position_angle
366 DATA runway_altitude, runway_latitude, runway_longitude, runway_heading;
367 #define Runway_altitude generic_.runway_altitude
368 #define Runway_latitude generic_.runway_latitude
369 #define Runway_longitude generic_.runway_longitude
370 #define Runway_heading generic_.runway_heading
373 #define Radius_to_rwy generic_.radius_to_rwy
375 VECTOR_3 d_cg_rwy_local_v; /* CG rel. to rwy in local coords */
376 #define D_cg_rwy_local_v generic_.d_cg_rwy_local_v
377 #define D_cg_north_of_rwy generic_.d_cg_rwy_local_v[0]
378 #define D_cg_east_of_rwy generic_.d_cg_rwy_local_v[1]
379 #define D_cg_above_rwy generic_.d_cg_rwy_local_v[2]
381 VECTOR_3 d_cg_rwy_rwy_v; /* CG relative to runway, in rwy coordinates */
382 #define D_cg_rwy_rwy_v generic_.d_cg_rwy_rwy_v
383 #define X_cg_rwy generic_.d_cg_rwy_rwy_v[0]
384 #define Y_cg_rwy generic_.d_cg_rwy_rwy_v[1]
385 #define H_cg_rwy generic_.d_cg_rwy_rwy_v[2]
387 VECTOR_3 d_pilot_rwy_local_v; /* pilot rel. to rwy in local coords */
388 #define D_pilot_rwy_local_v generic_.d_pilot_rwy_local_v
389 #define D_pilot_north_of_rwy generic_.d_pilot_rwy_local_v[0]
390 #define D_pilot_east_of_rwy generic_.d_pilot_rwy_local_v[1]
391 #define D_pilot_above_rwy generic_.d_pilot_rwy_local_v[2]
393 VECTOR_3 d_pilot_rwy_rwy_v; /* pilot rel. to rwy, in rwy coords. */
394 #define D_pilot_rwy_rwy_v generic_.d_pilot_rwy_rwy_v
395 #define X_pilot_rwy generic_.d_pilot_rwy_rwy_v[0]
396 #define Y_pilot_rwy generic_.d_pilot_rwy_rwy_v[1]
397 #define H_pilot_rwy generic_.d_pilot_rwy_rwy_v[2]
402 extern GENERIC generic_; /* usually defined in ls_main.c */
404 /*--------------------------- end of ls_generic.h ------------------------*/