23#ifndef FG_FLIGHT_PROPERTIES_HXX
24#define FG_FLIGHT_PROPERTIES_HXX
29#include <simgear/math/SGMathFwd.hxx>
30#include <simgear/math/SGMisc.hxx>
123 SGPropertyNode* _root;
double get_Phi_dot_degps() const
double get_A_X_pilot() const
void set_Euler_Angles(double phi, double theta, double psi)
double get_Phi_dot() const
void set_Velocities_Body(double x, double y, double z)
double get_Altitude_AGL(void) const
double get_V_east() const
double get_A_Y_pilot() const
void set_Velocities_Local(double x, double y, double z)
double get_V_calibrated_kts() const
double get_Total_pressure() const
void set_Altitude(double ft)
double get_Latitude_deg() const
double get_Runway_altitude_m() const
double get_Theta_dot_degps() const
void set_Climb_Rate(double fps)
void set_Latitude(double l)
double get_Q_body() const
double get_V_equiv_kts() const
double get_Longitude_deg() const
double get_Psi_deg() const
double get_Theta_deg() const
double get_V_down() const
double get_Track(void) const
void set_V_calibrated_kts(double kts)
double get_Latitude() const
double get_Psi_dot() const
double get_Phi_deg() const
void set_Euler_Rates(double x, double y, double z)
double get_Total_temperature() const
double get_V_ground_speed() const
double get_Longitude() const
double get_Theta_dot() const
double get_R_body() const
FlightProperties(SGPropertyNode *aRoot=NULL)
void set_Accels_Pilot_Body(double x, double y, double z)
double get_Dynamic_pressure() const
void set_Altitude_AGL(double ft)
SGGeod getPosition() const
double get_P_body() const
double get_V_north() const
double get_Climb_Rate() const
double get_Altitude() const
double get_Psi_dot_degps() const
void set_Longitude(double l)
double get_A_Z_pilot() const