Updates and tweaks for Oliver's multi-player networking code.
This commit is contained in:
curt
parent
bc6d6fbf50
commit
f89d86d4af
4 changed files with 203 additions and 135 deletions
|
|
@ -47,18 +47,49 @@ FGInterface *cur_fdm_state;
|
|||
FGInterface base_fdm_state;
|
||||
|
||||
|
||||
// Constructor
|
||||
FGInterface::FGInterface(void) {
|
||||
mass=i_xx=i_yy=i_zz=i_xz=0;
|
||||
nlf=0;
|
||||
v_rel_wind=v_true_kts=v_rel_ground=v_inertial=0;
|
||||
v_ground_speed=v_equiv=v_equiv_kts=0;
|
||||
v_calibrated=v_calibrated_kts=0;
|
||||
gravity=0;
|
||||
centrifugal_relief=0;
|
||||
alpha=beta=alpha_dot=beta_dot=0;
|
||||
cos_alpha=sin_alpha=cos_beta=sin_beta=0;
|
||||
cos_phi=sin_phi=cos_theta=sin_theta=cos_psi=sin_psi=0;
|
||||
gamma_vert_rad=gamma_horiz_rad=0;
|
||||
sigma=density=v_sound=mach_number=0;
|
||||
static_pressure=total_pressure=impact_pressure=0;
|
||||
dynamic_pressure=0;
|
||||
static_temperature=total_temperature=0;
|
||||
sea_level_radius=earth_position_angle=0;
|
||||
runway_altitude=runway_latitude=runway_longitude=0;
|
||||
runway_heading=0;
|
||||
radius_to_rwy=0;
|
||||
climb_rate=0;
|
||||
sin_lat_geocentric=cos_lat_geocentric=0;
|
||||
sin_longitude=cos_longitude=0;
|
||||
}
|
||||
|
||||
|
||||
// Destructor
|
||||
FGInterface::~FGInterface() {
|
||||
}
|
||||
|
||||
|
||||
int FGInterface::init( double dt ) {
|
||||
cout << "dummy init() ... SHOULDN'T BE CALLED!" << endl;
|
||||
return 0;
|
||||
}
|
||||
|
||||
|
||||
int FGInterface::update( int multi_loop ) {
|
||||
cout << "dummy update() ... SHOULDN'T BE CALLED!" << endl;
|
||||
return 0;
|
||||
}
|
||||
|
||||
FGInterface::~FGInterface() {
|
||||
}
|
||||
|
||||
// Extrapolate fdm based on time_offset (in usec)
|
||||
void FGInterface::extrapolate( int time_offset ) {
|
||||
|
|
|
|||
|
|
@ -25,9 +25,9 @@
|
|||
#define _FLIGHT_HXX
|
||||
|
||||
|
||||
#ifndef __cplusplus
|
||||
#ifndef __cplusplus
|
||||
# error This library requires C++
|
||||
#endif
|
||||
#endif
|
||||
|
||||
|
||||
/* Required get_()
|
||||
|
|
@ -92,28 +92,116 @@
|
|||
FG_USING_STD(list);
|
||||
|
||||
|
||||
#ifndef __cplusplus
|
||||
# error This library requires C++
|
||||
#endif
|
||||
|
||||
|
||||
typedef double FG_VECTOR_3[3];
|
||||
|
||||
|
||||
// This is based heavily on LaRCsim/ls_generic.h
|
||||
class FGInterface {
|
||||
|
||||
private:
|
||||
|
||||
// Pilot location rel to ref pt
|
||||
FG_VECTOR_3 d_pilot_rp_body_v;
|
||||
|
||||
// CG position w.r.t. ref. point
|
||||
FG_VECTOR_3 d_cg_rp_body_v;
|
||||
|
||||
// Forces
|
||||
FG_VECTOR_3 f_body_total_v;
|
||||
FG_VECTOR_3 f_local_total_v;
|
||||
FG_VECTOR_3 f_aero_v;
|
||||
FG_VECTOR_3 f_engine_v;
|
||||
FG_VECTOR_3 f_gear_v;
|
||||
|
||||
// Moments
|
||||
FG_VECTOR_3 m_total_rp_v;
|
||||
FG_VECTOR_3 m_total_cg_v;
|
||||
FG_VECTOR_3 m_aero_v;
|
||||
FG_VECTOR_3 m_engine_v;
|
||||
FG_VECTOR_3 m_gear_v;
|
||||
|
||||
// Accelerations
|
||||
FG_VECTOR_3 v_dot_local_v;
|
||||
FG_VECTOR_3 v_dot_body_v;
|
||||
FG_VECTOR_3 a_cg_body_v;
|
||||
FG_VECTOR_3 a_pilot_body_v;
|
||||
FG_VECTOR_3 n_cg_body_v;
|
||||
FG_VECTOR_3 n_pilot_body_v;
|
||||
FG_VECTOR_3 omega_dot_body_v;
|
||||
|
||||
// Velocities
|
||||
FG_VECTOR_3 v_local_v;
|
||||
FG_VECTOR_3 v_local_rel_ground_v; // V rel w.r.t. earth surface
|
||||
FG_VECTOR_3 v_local_airmass_v; // velocity of airmass (steady winds)
|
||||
FG_VECTOR_3 v_local_rel_airmass_v; // velocity of veh. relative to airmass
|
||||
FG_VECTOR_3 v_local_gust_v; // linear turbulence components, L frame
|
||||
FG_VECTOR_3 v_wind_body_v; // Wind-relative velocities in body axis
|
||||
|
||||
FG_VECTOR_3 omega_body_v; // Angular B rates
|
||||
FG_VECTOR_3 omega_local_v; // Angular L rates
|
||||
FG_VECTOR_3 omega_total_v; // Diff btw B & L
|
||||
FG_VECTOR_3 euler_rates_v;
|
||||
FG_VECTOR_3 geocentric_rates_v; // Geocentric linear velocities
|
||||
|
||||
// Positions
|
||||
FG_VECTOR_3 geocentric_position_v;
|
||||
FG_VECTOR_3 geodetic_position_v;
|
||||
FG_VECTOR_3 euler_angles_v;
|
||||
|
||||
// Miscellaneous Quantities
|
||||
FG_VECTOR_3 d_cg_rwy_local_v; // CG rel. to rwy in local coords
|
||||
FG_VECTOR_3 d_cg_rwy_rwy_v; // CG relative to rwy, in rwy coordinates
|
||||
FG_VECTOR_3 d_pilot_rwy_local_v; // pilot rel. to rwy in local coords
|
||||
FG_VECTOR_3 d_pilot_rwy_rwy_v; // pilot rel. to rwy, in rwy coords.
|
||||
|
||||
// Inertias
|
||||
double mass, i_xx, i_yy, i_zz, i_xz;
|
||||
|
||||
// Normal Load Factor
|
||||
double nlf;
|
||||
|
||||
// Velocities
|
||||
double v_rel_wind, v_true_kts, v_rel_ground, v_inertial;
|
||||
double v_ground_speed, v_equiv, v_equiv_kts;
|
||||
double v_calibrated, v_calibrated_kts;
|
||||
|
||||
// Miscellaneious Quantities
|
||||
double t_local_to_body_m[3][3]; // Transformation matrix L to B
|
||||
double gravity; // Local acceleration due to G
|
||||
double centrifugal_relief; // load factor reduction due to speed
|
||||
double alpha, beta, alpha_dot, beta_dot; // in radians
|
||||
double cos_alpha, sin_alpha, cos_beta, sin_beta;
|
||||
double cos_phi, sin_phi, cos_theta, sin_theta, cos_psi, sin_psi;
|
||||
double gamma_vert_rad, gamma_horiz_rad; // Flight path angles
|
||||
double sigma, density, v_sound, mach_number;
|
||||
double static_pressure, total_pressure, impact_pressure;
|
||||
double dynamic_pressure;
|
||||
double static_temperature, total_temperature;
|
||||
double sea_level_radius, earth_position_angle;
|
||||
double runway_altitude, runway_latitude, runway_longitude;
|
||||
double runway_heading;
|
||||
double radius_to_rwy;
|
||||
double climb_rate; // in feet per second
|
||||
double sin_lat_geocentric, cos_lat_geocentric;
|
||||
double sin_longitude, cos_longitude;
|
||||
double sin_latitude, cos_latitude;
|
||||
|
||||
FGTimeStamp valid_stamp; // time this record is valid
|
||||
FGTimeStamp next_stamp; // time this record is valid
|
||||
|
||||
public:
|
||||
|
||||
FGInterface(void);
|
||||
virtual ~FGInterface();
|
||||
|
||||
virtual int init( double dt );
|
||||
virtual int update( int multi_loop );
|
||||
virtual ~FGInterface();
|
||||
|
||||
// Define the various supported flight models (many not yet implemented)
|
||||
enum {
|
||||
// Magic Carpet mode
|
||||
FG_MAGICCARPET = 0,
|
||||
|
||||
|
||||
// The NASA LaRCsim (Navion) flight model
|
||||
FG_LARCSIM = 1,
|
||||
|
||||
|
|
@ -135,10 +223,9 @@ public:
|
|||
FG_EXTERNAL = 9
|
||||
};
|
||||
|
||||
/*================== Mass properties and geometry values ==================*/
|
||||
// ========== Mass properties and geometry values ==========
|
||||
|
||||
// Inertias
|
||||
double mass, i_xx, i_yy, i_zz, i_xz;
|
||||
inline double get_Mass() const { return mass; }
|
||||
inline double get_I_xx() const { return i_xx; }
|
||||
inline double get_I_yy() const { return i_yy; }
|
||||
|
|
@ -153,11 +240,10 @@ public:
|
|||
i_zz = zz;
|
||||
i_xz = xz;
|
||||
}
|
||||
|
||||
|
||||
// Pilot location rel to ref pt
|
||||
FG_VECTOR_3 d_pilot_rp_body_v;
|
||||
// inline double * get_D_pilot_rp_body_v() {
|
||||
// return d_pilot_rp_body_v;
|
||||
// inline double * get_D_pilot_rp_body_v() {
|
||||
// return d_pilot_rp_body_v;
|
||||
// }
|
||||
// inline double get_Dx_pilot() const { return d_pilot_rp_body_v[0]; }
|
||||
// inline double get_Dy_pilot() const { return d_pilot_rp_body_v[1]; }
|
||||
|
|
@ -169,7 +255,6 @@ public:
|
|||
} */
|
||||
|
||||
// CG position w.r.t. ref. point
|
||||
FG_VECTOR_3 d_cg_rp_body_v;
|
||||
// inline double * get_D_cg_rp_body_v() { return d_cg_rp_body_v; }
|
||||
inline double get_Dx_cg() const { return d_cg_rp_body_v[0]; }
|
||||
inline double get_Dy_cg() const { return d_cg_rp_body_v[1]; }
|
||||
|
|
@ -180,9 +265,8 @@ public:
|
|||
d_cg_rp_body_v[2] = dz;
|
||||
}
|
||||
|
||||
/*================================ Forces =================================*/
|
||||
// ========== Forces ==========
|
||||
|
||||
FG_VECTOR_3 f_body_total_v;
|
||||
// inline double * get_F_body_total_v() { return f_body_total_v; }
|
||||
// inline double get_F_X() const { return f_body_total_v[0]; }
|
||||
// inline double get_F_Y() const { return f_body_total_v[1]; }
|
||||
|
|
@ -193,7 +277,6 @@ public:
|
|||
f_body_total_v[2] = z;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 f_local_total_v;
|
||||
// inline double * get_F_local_total_v() { return f_local_total_v; }
|
||||
// inline double get_F_north() const { return f_local_total_v[0]; }
|
||||
// inline double get_F_east() const { return f_local_total_v[1]; }
|
||||
|
|
@ -204,7 +287,6 @@ public:
|
|||
f_local_total_v[2] = z;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 f_aero_v;
|
||||
// inline double * get_F_aero_v() { return f_aero_v; }
|
||||
// inline double get_F_X_aero() const { return f_aero_v[0]; }
|
||||
// inline double get_F_Y_aero() const { return f_aero_v[1]; }
|
||||
|
|
@ -215,7 +297,6 @@ public:
|
|||
f_aero_v[2] = z;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 f_engine_v;
|
||||
// inline double * get_F_engine_v() { return f_engine_v; }
|
||||
// inline double get_F_X_engine() const { return f_engine_v[0]; }
|
||||
// inline double get_F_Y_engine() const { return f_engine_v[1]; }
|
||||
|
|
@ -226,7 +307,6 @@ public:
|
|||
f_engine_v[2] = z;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 f_gear_v;
|
||||
// inline double * get_F_gear_v() { return f_gear_v; }
|
||||
// inline double get_F_X_gear() const { return f_gear_v[0]; }
|
||||
// inline double get_F_Y_gear() const { return f_gear_v[1]; }
|
||||
|
|
@ -237,9 +317,8 @@ public:
|
|||
f_gear_v[2] = z;
|
||||
} */
|
||||
|
||||
/*================================ Moments ================================*/
|
||||
// ========== Moments ==========
|
||||
|
||||
FG_VECTOR_3 m_total_rp_v;
|
||||
// inline double * get_M_total_rp_v() { return m_total_rp_v; }
|
||||
// inline double get_M_l_rp() const { return m_total_rp_v[0]; }
|
||||
// inline double get_M_m_rp() const { return m_total_rp_v[1]; }
|
||||
|
|
@ -250,7 +329,6 @@ public:
|
|||
m_total_rp_v[2] = n;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 m_total_cg_v;
|
||||
// inline double * get_M_total_cg_v() { return m_total_cg_v; }
|
||||
// inline double get_M_l_cg() const { return m_total_cg_v[0]; }
|
||||
// inline double get_M_m_cg() const { return m_total_cg_v[1]; }
|
||||
|
|
@ -261,7 +339,6 @@ public:
|
|||
m_total_cg_v[2] = n;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 m_aero_v;
|
||||
// inline double * get_M_aero_v() { return m_aero_v; }
|
||||
// inline double get_M_l_aero() const { return m_aero_v[0]; }
|
||||
// inline double get_M_m_aero() const { return m_aero_v[1]; }
|
||||
|
|
@ -272,7 +349,6 @@ public:
|
|||
m_aero_v[2] = n;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 m_engine_v;
|
||||
// inline double * get_M_engine_v() { return m_engine_v; }
|
||||
// inline double get_M_l_engine() const { return m_engine_v[0]; }
|
||||
// inline double get_M_m_engine() const { return m_engine_v[1]; }
|
||||
|
|
@ -283,7 +359,6 @@ public:
|
|||
m_engine_v[2] = n;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 m_gear_v;
|
||||
// inline double * get_M_gear_v() { return m_gear_v; }
|
||||
// inline double get_M_l_gear() const { return m_gear_v[0]; }
|
||||
// inline double get_M_m_gear() const { return m_gear_v[1]; }
|
||||
|
|
@ -294,9 +369,8 @@ public:
|
|||
m_gear_v[2] = n;
|
||||
} */
|
||||
|
||||
/*============================== Accelerations ============================*/
|
||||
// ========== Accelerations ==========
|
||||
|
||||
FG_VECTOR_3 v_dot_local_v;
|
||||
// inline double * get_V_dot_local_v() { return v_dot_local_v; }
|
||||
inline double get_V_dot_north() const { return v_dot_local_v[0]; }
|
||||
inline double get_V_dot_east() const { return v_dot_local_v[1]; }
|
||||
|
|
@ -307,7 +381,6 @@ public:
|
|||
v_dot_local_v[2] = down;
|
||||
}
|
||||
|
||||
FG_VECTOR_3 v_dot_body_v;
|
||||
// inline double * get_V_dot_body_v() { return v_dot_body_v; }
|
||||
inline double get_U_dot_body() const { return v_dot_body_v[0]; }
|
||||
inline double get_V_dot_body() const { return v_dot_body_v[1]; }
|
||||
|
|
@ -318,7 +391,6 @@ public:
|
|||
v_dot_body_v[2] = w;
|
||||
}
|
||||
|
||||
FG_VECTOR_3 a_cg_body_v;
|
||||
// inline double * get_A_cg_body_v() { return a_cg_body_v; }
|
||||
inline double get_A_X_cg() const { return a_cg_body_v[0]; }
|
||||
inline double get_A_Y_cg() const { return a_cg_body_v[1]; }
|
||||
|
|
@ -329,7 +401,6 @@ public:
|
|||
a_cg_body_v[2] = z;
|
||||
}
|
||||
|
||||
FG_VECTOR_3 a_pilot_body_v;
|
||||
// inline double * get_A_pilot_body_v() { return a_pilot_body_v; }
|
||||
inline double get_A_X_pilot() const { return a_pilot_body_v[0]; }
|
||||
inline double get_A_Y_pilot() const { return a_pilot_body_v[1]; }
|
||||
|
|
@ -340,7 +411,6 @@ public:
|
|||
a_pilot_body_v[2] = z;
|
||||
}
|
||||
|
||||
FG_VECTOR_3 n_cg_body_v;
|
||||
// inline double * get_N_cg_body_v() { return n_cg_body_v; }
|
||||
// inline double get_N_X_cg() const { return n_cg_body_v[0]; }
|
||||
// inline double get_N_Y_cg() const { return n_cg_body_v[1]; }
|
||||
|
|
@ -349,9 +419,8 @@ public:
|
|||
// n_cg_body_v[0] = x;
|
||||
// n_cg_body_v[1] = y;
|
||||
// n_cg_body_v[2] = z;
|
||||
// }
|
||||
// }
|
||||
|
||||
FG_VECTOR_3 n_pilot_body_v;
|
||||
// inline double * get_N_pilot_body_v() { return n_pilot_body_v; }
|
||||
// inline double get_N_X_pilot() const { return n_pilot_body_v[0]; }
|
||||
// inline double get_N_Y_pilot() const { return n_pilot_body_v[1]; }
|
||||
|
|
@ -360,13 +429,11 @@ public:
|
|||
// n_pilot_body_v[0] = x;
|
||||
// n_pilot_body_v[1] = y;
|
||||
// n_pilot_body_v[2] = z;
|
||||
// }
|
||||
|
||||
double nlf; //Normal Load Factor
|
||||
double get_Nlf(void) { return nlf; }
|
||||
// }
|
||||
|
||||
double get_Nlf(void) { return nlf; }
|
||||
void set_Nlf(double n) { nlf=n; }
|
||||
|
||||
FG_VECTOR_3 omega_dot_body_v;
|
||||
// inline double * get_Omega_dot_body_v() { return omega_dot_body_v; }
|
||||
// inline double get_P_dot_body() const { return omega_dot_body_v[0]; }
|
||||
// inline double get_Q_dot_body() const { return omega_dot_body_v[1]; }
|
||||
|
|
@ -378,9 +445,8 @@ public:
|
|||
} */
|
||||
|
||||
|
||||
/*============================== Velocities ===============================*/
|
||||
// ========== Velocities ==========
|
||||
|
||||
FG_VECTOR_3 v_local_v;
|
||||
// inline double * get_V_local_v() { return v_local_v; }
|
||||
inline double get_V_north() const { return v_local_v[0]; }
|
||||
inline double get_V_east() const { return v_local_v[1]; }
|
||||
|
|
@ -391,24 +457,25 @@ public:
|
|||
v_local_v[2] = down;
|
||||
}
|
||||
|
||||
FG_VECTOR_3 v_local_rel_ground_v; // V rel w.r.t. earth surface
|
||||
// inline double * get_V_local_rel_ground_v() { return v_local_rel_ground_v; }
|
||||
// inline double * get_V_local_rel_ground_v() {
|
||||
// return v_local_rel_ground_v;
|
||||
// }
|
||||
// inline double get_V_north_rel_ground() const {
|
||||
// return v_local_rel_ground_v[0];
|
||||
// }
|
||||
// return v_local_rel_ground_v[0];
|
||||
// }
|
||||
// inline double get_V_east_rel_ground() const {
|
||||
// return v_local_rel_ground_v[1];
|
||||
// }
|
||||
// return v_local_rel_ground_v[1];
|
||||
// }
|
||||
// inline double get_V_down_rel_ground() const {
|
||||
// return v_local_rel_ground_v[2];
|
||||
// }
|
||||
/* inline void set_Velocities_Ground(double north, double east, double down) {
|
||||
v_local_rel_ground_v[0] = north;
|
||||
v_local_rel_ground_v[1] = east;
|
||||
v_local_rel_ground_v[2] = down;
|
||||
} */
|
||||
// return v_local_rel_ground_v[2];
|
||||
// }
|
||||
// inline void set_Velocities_Ground(double north, double east, double down)
|
||||
// {
|
||||
// v_local_rel_ground_v[0] = north;
|
||||
// v_local_rel_ground_v[1] = east;
|
||||
// v_local_rel_ground_v[2] = down;
|
||||
// }
|
||||
|
||||
FG_VECTOR_3 v_local_airmass_v; // velocity of airmass (steady winds)
|
||||
// inline double * get_V_local_airmass_v() { return v_local_airmass_v; }
|
||||
inline double get_V_north_airmass() const { return v_local_airmass_v[0]; }
|
||||
inline double get_V_east_airmass() const { return v_local_airmass_v[1]; }
|
||||
|
|
@ -419,22 +486,21 @@ public:
|
|||
v_local_airmass_v[0] = north;
|
||||
v_local_airmass_v[1] = east;
|
||||
v_local_airmass_v[2] = down;
|
||||
}
|
||||
}
|
||||
|
||||
FG_VECTOR_3 v_local_rel_airmass_v; // velocity of veh. relative to
|
||||
// airmass
|
||||
// inline double * get_V_local_rel_airmass_v() {
|
||||
//return v_local_rel_airmass_v;
|
||||
//}
|
||||
// return v_local_rel_airmass_v;
|
||||
// }
|
||||
// inline double get_V_north_rel_airmass() const {
|
||||
//return v_local_rel_airmass_v[0];
|
||||
//}
|
||||
// return v_local_rel_airmass_v[0];
|
||||
// }
|
||||
// inline double get_V_east_rel_airmass() const {
|
||||
//return v_local_rel_airmass_v[1];
|
||||
//}
|
||||
// return v_local_rel_airmass_v[1];
|
||||
// }
|
||||
// inline double get_V_down_rel_airmass() const {
|
||||
//return v_local_rel_airmass_v[2];
|
||||
//}
|
||||
// return v_local_rel_airmass_v[2];
|
||||
// }
|
||||
/* inline void set_Velocities_Local_Rel_Airmass( double north, double east,
|
||||
double down)
|
||||
{
|
||||
|
|
@ -443,7 +509,6 @@ public:
|
|||
v_local_rel_airmass_v[2] = down;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 v_local_gust_v; // linear turbulence components, L frame
|
||||
// inline double * get_V_local_gust_v() { return v_local_gust_v; }
|
||||
// inline double get_U_gust() const { return v_local_gust_v[0]; }
|
||||
// inline double get_V_gust() const { return v_local_gust_v[1]; }
|
||||
|
|
@ -455,22 +520,16 @@ public:
|
|||
v_local_gust_v[2] = w;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 v_wind_body_v; // Wind-relative velocities in body axis
|
||||
// inline double * get_V_wind_body_v() { return v_wind_body_v; }
|
||||
inline double get_U_body() const { return v_wind_body_v[0]; }
|
||||
inline double get_V_body() const { return v_wind_body_v[1]; }
|
||||
inline double get_W_body() const { return v_wind_body_v[2]; }
|
||||
inline void set_Velocities_Wind_Body( double u, double v, double w)
|
||||
{
|
||||
inline void set_Velocities_Wind_Body( double u, double v, double w) {
|
||||
v_wind_body_v[0] = u;
|
||||
v_wind_body_v[1] = v;
|
||||
v_wind_body_v[2] = w;
|
||||
}
|
||||
|
||||
double v_rel_wind, v_true_kts, v_rel_ground, v_inertial;
|
||||
double v_ground_speed, v_equiv, v_equiv_kts;
|
||||
double v_calibrated, v_calibrated_kts;
|
||||
|
||||
// inline double get_V_rel_wind() const { return v_rel_wind; }
|
||||
// inline void set_V_rel_wind(double wind) { v_rel_wind = wind; }
|
||||
|
||||
|
|
@ -498,7 +557,6 @@ public:
|
|||
inline double get_V_calibrated_kts() const { return v_calibrated_kts; }
|
||||
inline void set_V_calibrated_kts( double kts ) { v_calibrated_kts = kts; }
|
||||
|
||||
FG_VECTOR_3 omega_body_v; // Angular B rates
|
||||
// inline double * get_Omega_body_v() { return omega_body_v; }
|
||||
inline double get_P_body() const { return omega_body_v[0]; }
|
||||
inline double get_Q_body() const { return omega_body_v[1]; }
|
||||
|
|
@ -509,7 +567,6 @@ public:
|
|||
omega_body_v[2] = r;
|
||||
}
|
||||
|
||||
FG_VECTOR_3 omega_local_v; // Angular L rates
|
||||
// inline double * get_Omega_local_v() { return omega_local_v; }
|
||||
// inline double get_P_local() const { return omega_local_v[0]; }
|
||||
// inline double get_Q_local() const { return omega_local_v[1]; }
|
||||
|
|
@ -520,7 +577,6 @@ public:
|
|||
omega_local_v[2] = r;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 omega_total_v; // Diff btw B & L
|
||||
// inline double * get_Omega_total_v() { return omega_total_v; }
|
||||
// inline double get_P_total() const { return omega_total_v[0]; }
|
||||
// inline double get_Q_total() const { return omega_total_v[1]; }
|
||||
|
|
@ -531,7 +587,6 @@ public:
|
|||
omega_total_v[2] = r;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 euler_rates_v;
|
||||
// inline double * get_Euler_rates_v() { return euler_rates_v; }
|
||||
inline double get_Phi_dot() const { return euler_rates_v[0]; }
|
||||
inline double get_Theta_dot() const { return euler_rates_v[1]; }
|
||||
|
|
@ -540,9 +595,8 @@ public:
|
|||
euler_rates_v[0] = phi;
|
||||
euler_rates_v[1] = theta;
|
||||
euler_rates_v[2] = psi;
|
||||
}
|
||||
}
|
||||
|
||||
FG_VECTOR_3 geocentric_rates_v; // Geocentric linear velocities
|
||||
// inline double * get_Geocentric_rates_v() { return geocentric_rates_v; }
|
||||
inline double get_Latitude_dot() const { return geocentric_rates_v[0]; }
|
||||
inline double get_Longitude_dot() const { return geocentric_rates_v[1]; }
|
||||
|
|
@ -552,17 +606,16 @@ public:
|
|||
geocentric_rates_v[1] = lon;
|
||||
geocentric_rates_v[2] = rad;
|
||||
}
|
||||
|
||||
/*=============================== Positions ===============================*/
|
||||
|
||||
FG_VECTOR_3 geocentric_position_v;
|
||||
// ========== Positions ==========
|
||||
|
||||
// inline double * get_Geocentric_position_v() {
|
||||
// return geocentric_position_v;
|
||||
// }
|
||||
inline double get_Lat_geocentric() const {
|
||||
return geocentric_position_v[0];
|
||||
}
|
||||
inline double get_Lon_geocentric() const {
|
||||
inline double get_Lon_geocentric() const {
|
||||
return geocentric_position_v[1];
|
||||
}
|
||||
inline double get_Radius_to_vehicle() const {
|
||||
|
|
@ -578,7 +631,6 @@ public:
|
|||
geocentric_position_v[2] = rad;
|
||||
}
|
||||
|
||||
FG_VECTOR_3 geodetic_position_v;
|
||||
// inline double * get_Geodetic_position_v() { return geodetic_position_v; }
|
||||
inline double get_Latitude() const { return geodetic_position_v[0]; }
|
||||
inline void set_Latitude(double lat) { geodetic_position_v[0] = lat; }
|
||||
|
|
@ -594,7 +646,6 @@ public:
|
|||
geodetic_position_v[2] = alt;
|
||||
}
|
||||
|
||||
FG_VECTOR_3 euler_angles_v;
|
||||
// inline double * get_Euler_angles_v() { return euler_angles_v; }
|
||||
inline double get_Phi() const { return euler_angles_v[0]; }
|
||||
inline double get_Theta() const { return euler_angles_v[1]; }
|
||||
|
|
@ -606,9 +657,8 @@ public:
|
|||
}
|
||||
|
||||
|
||||
/*======================= Miscellaneous quantities ========================*/
|
||||
// ========== Miscellaneous quantities ==========
|
||||
|
||||
double t_local_to_body_m[3][3]; // Transformation matrix L to B
|
||||
// inline double * get_T_local_to_body_m() { return t_local_to_body_m; }
|
||||
inline double get_T_local_to_body_11() const {
|
||||
return t_local_to_body_m[0][0];
|
||||
|
|
@ -638,8 +688,8 @@ public:
|
|||
return t_local_to_body_m[2][2];
|
||||
}
|
||||
inline void set_T_Local_to_Body( int i, int j, double value) {
|
||||
t_local_to_body_m[i-1][j-1] = value;
|
||||
}
|
||||
t_local_to_body_m[i-1][j-1] = value;
|
||||
}
|
||||
inline void set_T_Local_to_Body( double m[3][3] ) {
|
||||
int i, j;
|
||||
for ( i = 0; i < 3; i++ ) {
|
||||
|
|
@ -649,15 +699,16 @@ public:
|
|||
}
|
||||
}
|
||||
|
||||
double gravity; // Local acceleration due to G
|
||||
// inline double get_Gravity() const { return gravity; }
|
||||
// inline void set_Gravity(double g) { gravity = g; }
|
||||
|
||||
double centrifugal_relief; // load factor reduction due to speed
|
||||
// inline double get_Centrifugal_relief() const { return centrifugal_relief; }
|
||||
// inline void set_Centrifugal_relief(double cr) { centrifugal_relief = cr; }
|
||||
|
||||
double alpha, beta, alpha_dot, beta_dot; // in radians
|
||||
// inline double get_Centrifugal_relief() const {
|
||||
// return centrifugal_relief;
|
||||
// }
|
||||
// inline void set_Centrifugal_relief(double cr) {
|
||||
// centrifugal_relief = cr;
|
||||
// }
|
||||
|
||||
inline double get_Alpha() const { return alpha; }
|
||||
inline void set_Alpha( double a ) { alpha = a; }
|
||||
inline double get_Beta() const { return beta; }
|
||||
|
|
@ -667,7 +718,6 @@ public:
|
|||
// inline double get_Beta_dot() const { return beta_dot; }
|
||||
// inline void set_Beta_dot( double bd ) { beta_dot = bd; }
|
||||
|
||||
double cos_alpha, sin_alpha, cos_beta, sin_beta;
|
||||
// inline double get_Cos_alpha() const { return cos_alpha; }
|
||||
// inline void set_Cos_alpha( double ca ) { cos_alpha = ca; }
|
||||
// inline double get_Sin_alpha() const { return sin_alpha; }
|
||||
|
|
@ -677,7 +727,6 @@ public:
|
|||
// inline double get_Sin_beta() const { return sin_beta; }
|
||||
// inline void set_Sin_beta( double sb ) { sin_beta = sb; }
|
||||
|
||||
double cos_phi, sin_phi, cos_theta, sin_theta, cos_psi, sin_psi;
|
||||
inline double get_Cos_phi() const { return cos_phi; }
|
||||
inline void set_Cos_phi( double cp ) { cos_phi = cp; }
|
||||
// inline double get_Sin_phi() const { return sin_phi; }
|
||||
|
|
@ -691,13 +740,11 @@ public:
|
|||
// inline double get_Sin_psi() const { return sin_psi; }
|
||||
// inline void set_Sin_psi( double sp ) { sin_psi = sp; }
|
||||
|
||||
double gamma_vert_rad, gamma_horiz_rad; // Flight path angles
|
||||
inline double get_Gamma_vert_rad() const { return gamma_vert_rad; }
|
||||
inline void set_Gamma_vert_rad( double gv ) { gamma_vert_rad = gv; }
|
||||
// inline double get_Gamma_horiz_rad() const { return gamma_horiz_rad; }
|
||||
// inline void set_Gamma_horiz_rad( double gh ) { gamma_horiz_rad = gh; }
|
||||
|
||||
double sigma, density, v_sound, mach_number;
|
||||
// inline double get_Sigma() const { return sigma; }
|
||||
// inline void set_Sigma( double s ) { sigma = s; }
|
||||
inline double get_Density() const { return density; }
|
||||
|
|
@ -707,8 +754,6 @@ public:
|
|||
inline double get_Mach_number() const { return mach_number; }
|
||||
inline void set_Mach_number( double m ) { mach_number = m; }
|
||||
|
||||
double static_pressure, total_pressure, impact_pressure;
|
||||
double dynamic_pressure;
|
||||
inline double get_Static_pressure() const { return static_pressure; }
|
||||
inline void set_Static_pressure( double sp ) { static_pressure = sp; }
|
||||
// inline double get_Total_pressure() const { return total_pressure; }
|
||||
|
|
@ -718,41 +763,41 @@ public:
|
|||
// inline double get_Dynamic_pressure() const { return dynamic_pressure; }
|
||||
// inline void set_Dynamic_pressure( double dp ) { dynamic_pressure = dp; }
|
||||
|
||||
double static_temperature, total_temperature;
|
||||
inline double get_Static_temperature() const { return static_temperature; }
|
||||
inline void set_Static_temperature( double t ) { static_temperature = t; }
|
||||
// inline double get_Total_temperature() const { return total_temperature; }
|
||||
// inline void set_Total_temperature( double t ) { total_temperature = t; }
|
||||
|
||||
double sea_level_radius, earth_position_angle;
|
||||
inline double get_Sea_level_radius() const { return sea_level_radius; }
|
||||
inline void set_Sea_level_radius( double r ) { sea_level_radius = r; }
|
||||
inline double get_Earth_position_angle() const {
|
||||
return earth_position_angle;
|
||||
}
|
||||
inline void set_Earth_position_angle(double a) {
|
||||
inline void set_Earth_position_angle(double a) {
|
||||
earth_position_angle = a;
|
||||
}
|
||||
|
||||
double runway_altitude, runway_latitude, runway_longitude;
|
||||
double runway_heading;
|
||||
inline double get_Runway_altitude() const { return runway_altitude; }
|
||||
inline void set_Runway_altitude( double alt ) { runway_altitude = alt; }
|
||||
// inline double get_Runway_latitude() const { return runway_latitude; }
|
||||
// inline void set_Runway_latitude( double lat ) { runway_latitude = lat; }
|
||||
// inline double get_Runway_longitude() const { return runway_longitude; }
|
||||
// inline void set_Runway_longitude( double lon ) { runway_longitude = lon; }
|
||||
// inline void set_Runway_longitude( double lon ) {
|
||||
// runway_longitude = lon;
|
||||
// }
|
||||
// inline double get_Runway_heading() const { return runway_heading; }
|
||||
// inline void set_Runway_heading( double h ) { runway_heading = h; }
|
||||
|
||||
double radius_to_rwy;
|
||||
// inline double get_Radius_to_rwy() const { return radius_to_rwy; }
|
||||
// inline void set_Radius_to_rwy( double r ) { radius_to_rwy = r; }
|
||||
|
||||
FG_VECTOR_3 d_cg_rwy_local_v; // CG rel. to rwy in local coords
|
||||
// inline double * get_D_cg_rwy_local_v() { return d_cg_rwy_local_v; }
|
||||
// inline double get_D_cg_north_of_rwy() const { return d_cg_rwy_local_v[0]; }
|
||||
// inline double get_D_cg_east_of_rwy() const { return d_cg_rwy_local_v[1]; }
|
||||
// inline double get_D_cg_north_of_rwy() const {
|
||||
// return d_cg_rwy_local_v[0];
|
||||
// }
|
||||
// inline double get_D_cg_east_of_rwy() const {
|
||||
// return d_cg_rwy_local_v[1];
|
||||
// }
|
||||
// inline double get_D_cg_above_rwy() const { return d_cg_rwy_local_v[2]; }
|
||||
/* inline void set_CG_Rwy_Local( double north, double east, double above )
|
||||
{
|
||||
|
|
@ -761,7 +806,6 @@ public:
|
|||
d_cg_rwy_local_v[2] = above;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 d_cg_rwy_rwy_v; // CG relative to rwy, in rwy coordinates
|
||||
// inline double * get_D_cg_rwy_rwy_v() { return d_cg_rwy_rwy_v; }
|
||||
// inline double get_X_cg_rwy() const { return d_cg_rwy_rwy_v[0]; }
|
||||
// inline double get_Y_cg_rwy() const { return d_cg_rwy_rwy_v[1]; }
|
||||
|
|
@ -773,17 +817,16 @@ public:
|
|||
d_cg_rwy_rwy_v[2] = h;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 d_pilot_rwy_local_v; // pilot rel. to rwy in local coords
|
||||
// inline double * get_D_pilot_rwy_local_v() { return d_pilot_rwy_local_v; }
|
||||
// inline double get_D_pilot_north_of_rwy() const {
|
||||
//return d_pilot_rwy_local_v[0];
|
||||
// }
|
||||
// return d_pilot_rwy_local_v[0];
|
||||
// }
|
||||
// inline double get_D_pilot_east_of_rwy() const {
|
||||
// return d_pilot_rwy_local_v[1];
|
||||
// }
|
||||
// return d_pilot_rwy_local_v[1];
|
||||
// }
|
||||
// inline double get_D_pilot_above_rwy() const {
|
||||
//return d_pilot_rwy_local_v[2];
|
||||
// }
|
||||
// return d_pilot_rwy_local_v[2];
|
||||
// }
|
||||
/* inline void set_Pilot_Rwy_Local( double north, double east, double above )
|
||||
{
|
||||
d_pilot_rwy_local_v[0] = north;
|
||||
|
|
@ -791,7 +834,6 @@ public:
|
|||
d_pilot_rwy_local_v[2] = above;
|
||||
} */
|
||||
|
||||
FG_VECTOR_3 d_pilot_rwy_rwy_v; // pilot rel. to rwy, in rwy coords.
|
||||
// inline double * get_D_pilot_rwy_rwy_v() { return d_pilot_rwy_rwy_v; }
|
||||
// inline double get_X_pilot_rwy() const { return d_pilot_rwy_rwy_v[0]; }
|
||||
// inline double get_Y_pilot_rwy() const { return d_pilot_rwy_rwy_v[1]; }
|
||||
|
|
@ -803,12 +845,9 @@ public:
|
|||
d_pilot_rwy_rwy_v[2] = h;
|
||||
} */
|
||||
|
||||
double climb_rate; // in feet per second
|
||||
inline double get_Climb_Rate() const { return climb_rate; }
|
||||
inline void set_Climb_Rate(double rate) { climb_rate = rate; }
|
||||
|
||||
FGTimeStamp valid_stamp; // time this record is valid
|
||||
FGTimeStamp next_stamp; // time this record is valid
|
||||
inline FGTimeStamp get_time_stamp() const { return valid_stamp; }
|
||||
inline void stamp_time() { valid_stamp = next_stamp; next_stamp.stamp(); }
|
||||
|
||||
|
|
@ -816,8 +855,6 @@ public:
|
|||
void extrapolate( int time_offset );
|
||||
|
||||
// sin/cos lat_geocentric
|
||||
double sin_lat_geocentric;
|
||||
double cos_lat_geocentric;
|
||||
inline void set_sin_lat_geocentric(double parm) {
|
||||
sin_lat_geocentric = sin(parm);
|
||||
}
|
||||
|
|
@ -831,8 +868,6 @@ public:
|
|||
return cos_lat_geocentric;
|
||||
}
|
||||
|
||||
double sin_longitude;
|
||||
double cos_longitude;
|
||||
inline void set_sin_cos_longitude(double parm) {
|
||||
sin_longitude = sin(parm);
|
||||
cos_longitude = cos(parm);
|
||||
|
|
@ -843,9 +878,7 @@ public:
|
|||
inline double get_cos_longitude(void) const {
|
||||
return cos_longitude;
|
||||
}
|
||||
|
||||
double sin_latitude;
|
||||
double cos_latitude;
|
||||
|
||||
inline void set_sin_cos_latitude(double parm) {
|
||||
sin_latitude = sin(parm);
|
||||
cos_latitude = cos(parm);
|
||||
|
|
|
|||
|
|
@ -1560,7 +1560,9 @@ void guiInit()
|
|||
mainMenuBar -> add_submenu ("Environment", environmentSubmenu, environmentSubmenuCb);
|
||||
// mainMenuBar -> add_submenu ("Options", optionsSubmenu, optionsSubmenuCb);
|
||||
#ifdef FG_NETWORK_OLK
|
||||
mainMenuBar -> add_submenu ("Network", networkSubmenu, networkSubmenuCb);
|
||||
if ( current_options.get_network_olk() ) {
|
||||
mainMenuBar -> add_submenu ("Network", networkSubmenu, networkSubmenuCb);
|
||||
}
|
||||
#endif
|
||||
mainMenuBar -> add_submenu ("Help", helpSubmenu, helpSubmenuCb);
|
||||
mainMenuBar-> close ();
|
||||
|
|
|
|||
|
|
@ -1044,6 +1044,8 @@ void fgOPTIONS::usage ( void ) {
|
|||
cout << "" << endl;
|
||||
|
||||
cout << "Network Options:" << endl;
|
||||
cout << "\t--enable-network-olk: enable Multipilot mode" << endl;
|
||||
cout << "\t--disable-network-olk: disable Multipilot mode (default)" << endl;
|
||||
cout << "\t--net-hud: Hud displays network info" << endl;
|
||||
cout << "\t--net-id=name: specify your own callsign" << endl;
|
||||
#endif
|
||||
|
|
|
|||
Loading…
Add table
Reference in a new issue