Searched refs:Std_Beta (Results 1 – 15 of 15) sorted by relevance
395 CZclean_wing += CZ_deb2_clean * elevator * Std_Beta * Std_Beta; in uiuc_coef_lift()396 CZclean_tail += CZ_deb2_clean * elevator * Std_Beta * Std_Beta; in uiuc_coef_lift()397 CZiced_wing += CZ_deb2 * elevator * Std_Beta * Std_Beta; in uiuc_coef_lift()398 CZiced_tail += CZ_deb2 * elevator * Std_Beta * Std_Beta; in uiuc_coef_lift()401 CZ_deb2_save = CZ_deb2 * elevator * Std_Beta * Std_Beta; in uiuc_coef_lift()460 Std_Beta); in uiuc_coef_lift()471 Std_Beta); in uiuc_coef_lift()
125 Cn_beta_save = Cn_beta * Std_Beta; in uiuc_coef_yaw()217 Cn_b3_save = Cn_b3 * Std_Beta * Std_Beta * Std_Beta; in uiuc_coef_yaw()240 Std_Beta, in uiuc_coef_yaw()257 Std_Beta); in uiuc_coef_yaw()268 Std_Beta); in uiuc_coef_yaw()
125 CY_beta_save = CY_beta * Std_Beta; in uiuc_coef_sideforce()240 Std_Beta, in uiuc_coef_sideforce()257 Std_Beta); in uiuc_coef_sideforce()268 Std_Beta); in uiuc_coef_sideforce()
125 Cl_beta_save = Cl_beta * Std_Beta; in uiuc_coef_roll()236 Std_Beta, in uiuc_coef_roll()253 Std_Beta); in uiuc_coef_roll()264 Std_Beta); in uiuc_coef_roll()
204 Cm_b2_save = Cm_b2 * Std_Beta * Std_Beta; in uiuc_coef_pitch()332 Std_Beta); in uiuc_coef_pitch()343 Std_Beta); in uiuc_coef_pitch()
199 CD_beta_save = fabs(CD_beta * Std_Beta); in uiuc_coef_drag()475 Std_Beta); in uiuc_coef_drag()498 Std_Beta); in uiuc_coef_drag()
111 Std_Beta = Beta_init; in uiuc_coefficients()
624 fout << Std_Beta << " "; in uiuc_recorder()629 fout << Std_Beta * RAD_TO_DEG << " "; in uiuc_recorder()
145 Cl = Clb*Std_Beta + Clp*(p*b/2.0/V) + Clr*(r*b/2.0/V) + Clda * aileron; in cherokee_aero()147 Cy = Cyb*Std_Beta + Cyr*(r*b/2.0/V); in cherokee_aero()148 Cn = Cnb*Std_Beta + Cnp*(p*b/2.0/V) + Cnr*(r*b/2.0/V) + Cndr * rudder; in cherokee_aero()
394 Std_Beta = 0; in ls_aux()396 Std_Beta = asin( V_body/ V_rel_wind ); in ls_aux()398 Cos_beta = cos(Std_Beta); in ls_aux()399 Sin_beta = sin(Std_Beta); in ls_aux()
442 Cl_w = Cl_b*Std_Beta + Cl_p*Phat + Cl_r_mod*Rhat in basic_aero()453 Cy_drela = CY_b*Std_Beta + CY_p*Phat + CY_r*Rhat + CY_dr*rudder; in basic_aero()456 Cl_drela = Cl_b*Std_Beta + Cl_p*Phat + Cl_r_mod*Rhat + Cl_dr*rudder in basic_aero()458 Cn_drela = Cn_b*Std_Beta + Cn_p_mod*Phat + Cn_r*Rhat + Cn_dr*rudder in basic_aero()
205 M_l_aero = scale*(I_xx*(L_beta*Std_Beta + L_p*P_body + L_r*R_body in navion_aero()208 M_n_aero = scale*(I_zz*(N_beta*Std_Beta + N_p*P_body + N_r*R_body in navion_aero()
441 cy = Cybeta*Std_Beta + (Cyp*P_body + Cyr*R_body)*b_2V + Cyda*aileron + Cydr*rudder; in c172_aero()444 cn = Cnbeta*Std_Beta + (Cnp*P_body + Cnr*R_body)*b_2V + Cnda*aileron + Cndr*rudder; in c172_aero()445 croll=Clbeta*Std_Beta + (Clp*P_body + Clr*R_body)*b_2V + Clda*aileron + Cldr*rudder; in c172_aero()
340 #define Std_Beta generic_.beta macro
705 _set_Beta( Std_Beta ); in copy_from_LaRCsim()