| Aero_t1 | Aircraft | |
| Aero_t2 | Aircraft | |
| Aero_torque | Aircraft | |
| aircraft | Aircraft | |
| Aircraft(const std::string &fname, int &vehicle_count) | Aircraft | |
| aircraft_scale | Aircraft | |
| alpha | Aircraft | |
| alpha0 | Aircraft | |
| animate(easy3d::Viewer *viewer, double dt) | Aircraft | |
| axes_vertices | Aircraft | |
| axes_vertices_original | Aircraft | |
| axesDrawable | Aircraft | |
| beta | Aircraft | |
| beta0 | Aircraft | |
| C_D_0 | Aircraft | |
| C_D_alpha | Aircraft | |
| C_D_delta_e | Aircraft | |
| C_D_p | Aircraft | |
| C_D_q | Aircraft | |
| C_ell_0 | Aircraft | |
| C_ell_beta | Aircraft | |
| C_ell_delta_a | Aircraft | |
| C_ell_delta_r | Aircraft | |
| C_ell_p | Aircraft | |
| C_ell_r | Aircraft | |
| C_L_0 | Aircraft | |
| C_L_alpha | Aircraft | |
| C_L_delta_e | Aircraft | |
| C_L_q | Aircraft | |
| C_m_0 | Aircraft | |
| C_m_alpha | Aircraft | |
| C_m_delta_e | Aircraft | |
| C_m_q | Aircraft | |
| C_n_0 | Aircraft | |
| C_n_beta | Aircraft | |
| C_n_delta_a | Aircraft | |
| C_n_delta_r | Aircraft | |
| C_n_p | Aircraft | |
| C_n_r | Aircraft | |
| C_p_0 | Aircraft | |
| C_p_beta | Aircraft | |
| C_p_delta_a | Aircraft | |
| C_p_delta_r | Aircraft | |
| C_p_p | Aircraft | |
| C_p_r | Aircraft | |
| C_prop | Aircraft | |
| C_r_0 | Aircraft | |
| C_r_beta | Aircraft | |
| C_r_delta_a | Aircraft | |
| C_r_delta_r | Aircraft | |
| C_r_p | Aircraft | |
| C_r_r | Aircraft | |
| C_Y_0 | Aircraft | |
| C_Y_beta | Aircraft | |
| C_Y_delta_a | Aircraft | |
| C_Y_delta_r | Aircraft | |
| C_Y_p | Aircraft | |
| C_Y_r | Aircraft | |
| calculate_body_frame_velocity_and_angles() | Aircraft | private |
| calculate_forces() | Aircraft | private |
| calculate_lift_drag_coefficients() | Aircraft | private |
| calculate_moments() | Aircraft | private |
| calculate_p_dot(double &p, double &q, double &r, double &ell, double &n, double &Gamma_1, double &Gamma_2, double &Gamma_3, double &Gamma_4) | Aircraft | private |
| calculate_pd_dot(double &u, double &v, double &w, double &phi, double &theta) | Aircraft | private |
| calculate_pe_dot(double &u, double &v, double &w, double &phi, double &theta, double &psi) | Aircraft | private |
| calculate_phi_dot(double &p, double &q, double &r, double &phi, double &theta) | Aircraft | private |
| calculate_pn_dot(double &u, double &v, double &w, double &phi, double &theta, double &psi) | Aircraft | private |
| calculate_psi_dot(double &q, double &r, double &phi, double &theta) | Aircraft | private |
| calculate_q_dot(double &p, double &r, double &m, double &Jy, double &Gamma_5, double &Gamma_6) | Aircraft | private |
| calculate_r_dot(double &p, double &q, double &r, double &ell, double &n, double &Gamma_1, double &Gamma_4, double &Gamma_7, double &Gamma_8) | Aircraft | private |
| calculate_theta_dot(double &q, double &r, double &phi) | Aircraft | private |
| calculate_u_dot(double &v, double &w, double &q, double &r, double &fx, double &mass) | Aircraft | private |
| calculate_v_dot(double &u, double &w, double &p, double &fy, double &mass) | Aircraft | private |
| calculate_w_dot(double &u, double &v, double &p, double &q, double &fz, double &mass) | Aircraft | private |
| Cd_of_alpha | Aircraft | |
| Cl_flat_plate | Aircraft | |
| Cl_linear | Aircraft | |
| Cl_of_alpha | Aircraft | |
| clock | Aircraft | |
| computeStateDot(const Eigen::VectorXd &X_in, const Eigen::VectorXd &U_in) | Aircraft | |
| computeTrimControls(double alpha, double beta, double phi, double p, double q, double r, double theta, double Va, double R) | Aircraft | |
| createAxesDrawable(easy3d::Viewer &viewer) | Aircraft | |
| CxAlpha | Aircraft | |
| CxdeltaeAlpha | Aircraft | |
| CxqAlpha | Aircraft | |
| CzAlpha | Aircraft | |
| CzdeltaeAlpha | Aircraft | |
| CzqAlpha | Aircraft | |
| delta_a | Aircraft | |
| delta_a_max | Aircraft | |
| delta_a_min | Aircraft | |
| delta_e | Aircraft | |
| delta_e_max | Aircraft | |
| delta_e_min | Aircraft | |
| delta_r | Aircraft | |
| delta_r_max | Aircraft | |
| delta_r_min | Aircraft | |
| delta_t | Aircraft | |
| delta_t_max | Aircraft | |
| delta_t_min | Aircraft | |
| dt | Aircraft | |
| dummy_points | Aircraft | |
| e | Aircraft | |
| ell | Aircraft | |
| epsilon | Aircraft | |
| faces | Aircraft | |
| file_name | Aircraft | |
| Force | Aircraft | |
| force_aero | Aircraft | |
| force_aero1 | Aircraft | |
| force_aero2 | Aircraft | |
| force_g | Aircraft | |
| force_prop | Aircraft | |
| force_prop1 | Aircraft | |
| force_prop2 | Aircraft | |
| fx | Aircraft | |
| fy | Aircraft | |
| fz | Aircraft | |
| g | Aircraft | |
| Gamma | Aircraft | |
| Gamma_1 | Aircraft | |
| Gamma_2 | Aircraft | |
| Gamma_3 | Aircraft | |
| Gamma_4 | Aircraft | |
| Gamma_5 | Aircraft | |
| Gamma_6 | Aircraft | |
| Gamma_7 | Aircraft | |
| Gamma_8 | Aircraft | |
| getAircraftDrawable() const | Aircraft | inline |
| getLateralState() const | Aircraft | |
| getLongitudinalState() const | Aircraft | |
| GNC | Aircraft | friend |
| id | Aircraft | |
| indices | Aircraft | |
| Jx | Aircraft | |
| Jxz | Aircraft | |
| Jy | Aircraft | |
| Jz | Aircraft | |
| k_motor | Aircraft | |
| load_a_plane(const std::string &filePath, int &vehicle_count) | Aircraft | |
| m | Aircraft | |
| mass | Aircraft | |
| mesh | Aircraft | |
| n | Aircraft | |
| old_pd | Aircraft | |
| old_pe | Aircraft | |
| old_pitch | Aircraft | |
| old_pn | Aircraft | |
| old_roll | Aircraft | |
| old_yaw | Aircraft | |
| original_vertices | Aircraft | |
| p | Aircraft | |
| p_0 | Aircraft | |
| p_dot | Aircraft | |
| pd | Aircraft | |
| pd_0 | Aircraft | |
| pd_dot | Aircraft | |
| pe | Aircraft | |
| pe_0 | Aircraft | |
| pe_dot | Aircraft | |
| phi | Aircraft | |
| phi_0 | Aircraft | |
| phi_dot | Aircraft | |
| pn | Aircraft | |
| pn_0 | Aircraft | |
| pn_dot | Aircraft | |
| points | Aircraft | |
| printState() | Aircraft | |
| prop_area | Aircraft | |
| prop_efficiency | Aircraft | |
| prop_omega | Aircraft | |
| prop_thrust_coef | Aircraft | |
| Prop_torque | Aircraft | |
| psi | Aircraft | |
| psi_0 | Aircraft | |
| psi_dot | Aircraft | |
| q | Aircraft | |
| q_0 | Aircraft | |
| q_dot | Aircraft | |
| r | Aircraft | |
| r_0 | Aircraft | |
| r_dot | Aircraft | |
| render_HUD(easy3d::TextRenderer &tr, easy3d::Viewer *viewer) const | Aircraft | |
| renderAircraft(easy3d::Viewer &viewer) | Aircraft | |
| rho | Aircraft | |
| RK4(std::vector< double > &X, double dt) | Aircraft | private |
| rotate(easy3d::vec3 *vertices) | Aircraft | private |
| rotate_axes(easy3d::vec3 *axesVertices) | Aircraft | private |
| sigma_den | Aircraft | |
| sigma_num | Aircraft | |
| sigma_of_alpha | Aircraft | |
| steps | Aircraft | |
| theta | Aircraft | |
| theta_0 | Aircraft | |
| theta_dot | Aircraft | |
| Torque | Aircraft | |
| trans_rate | Aircraft | |
| translate(easy3d::vec3 *vertices) | Aircraft | private |
| translate_axes(easy3d::vec3 *axesVertices) | Aircraft | private |
| u | Aircraft | |
| u_0 | Aircraft | |
| u_dot | Aircraft | |
| update_aircraft(easy3d::vec3 *vertices, easy3d::vec3 *axesVertices, double &dt) | Aircraft | |
| v | Aircraft | |
| v_0 | Aircraft | |
| v_dot | Aircraft | |
| V_m | Aircraft | |
| velocity_b | Aircraft | |
| vertices_aircraft | Aircraft | |
| vertices_size | Aircraft | |
| vertices_x | Aircraft | |
| vertices_y | Aircraft | |
| vertices_z | Aircraft | |
| w | Aircraft | |
| w_0 | Aircraft | |
| w_dot | Aircraft | |
| wing_area | Aircraft | |
| wing_aspect_ratio | Aircraft | |
| wing_chord | Aircraft | |
| wing_span | Aircraft | |
| X | Aircraft | |
| ~Aircraft() | Aircraft | |