flight_gear.h

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#ifndef FLIGHT_GEAR_H
#define FLIGHT_GEAR_H
 
#include <stdint.h>
 
#define FG_NET_CTRLS_VERSION 27
#define FG_NET_CTRLS_MAX_ENGINES 4
#define FG_NET_CTRLS_MAX_WHEELS  16
#define FG_NET_CTRLS_MAX_TANKS   8
#define FG_NET_CTRLS_RESERVED_SPACE 25
 
struct FGNetCtrls {
    uint32_t version;            // increment when data values change
 
    // Aero controls
    double aileron;            // -1 ... 1
    double elevator;             // -1 ... 1
    double rudder;             // -1 ... 1
    double aileron_trim;           // -1 ... 1
    double elevator_trim;          // -1 ... 1
    double rudder_trim;            // -1 ... 1
    double flaps;            //  0 ... 1
    double spoilers;
    double speedbrake;
 
    // Aero control faults
    uint32_t flaps_power;                 // true = power available
    uint32_t flap_motor_ok;
 
    // Engine controls
    uint32_t num_engines;    // number of valid engines
    uint32_t master_bat[FG_NET_CTRLS_MAX_ENGINES];
    uint32_t master_alt[FG_NET_CTRLS_MAX_ENGINES];
    uint32_t magnetos[FG_NET_CTRLS_MAX_ENGINES];
    uint32_t starter_power[FG_NET_CTRLS_MAX_ENGINES];// true = starter power
    double throttle[FG_NET_CTRLS_MAX_ENGINES];     //  0 ... 1
    double mixture[FG_NET_CTRLS_MAX_ENGINES];      //  0 ... 1
    double condition[FG_NET_CTRLS_MAX_ENGINES];    //  0 ... 1
    uint32_t fuel_pump_power[FG_NET_CTRLS_MAX_ENGINES];// true = on
    double prop_advance[FG_NET_CTRLS_MAX_ENGINES]; //  0 ... 1
    uint32_t feed_tank_to[4];
    uint32_t reverse[4];
 
    // Engine faults
    uint32_t engine_ok[FG_NET_CTRLS_MAX_ENGINES];
    uint32_t mag_left_ok[FG_NET_CTRLS_MAX_ENGINES];
    uint32_t mag_right_ok[FG_NET_CTRLS_MAX_ENGINES];
    uint32_t spark_plugs_ok[FG_NET_CTRLS_MAX_ENGINES];  // false = fouled plugs
    uint32_t oil_press_status[FG_NET_CTRLS_MAX_ENGINES];// 0 = normal, 1 = low, 2 = full fail
    uint32_t fuel_pump_ok[FG_NET_CTRLS_MAX_ENGINES];
 
    // Fuel management
    uint32_t num_tanks;                      // number of valid tanks
    uint32_t fuel_selector[FG_NET_CTRLS_MAX_TANKS];    // false = off, true = on
    uint32_t xfer_pump[5];                   // specifies transfer from array
                                             // value tank to tank specified by
                                             // int value
    uint32_t cross_feed;                     // false = off, true = on
 
    // Brake controls
    double brake_left;
    double brake_right;
    double copilot_brake_left;
    double copilot_brake_right;
    double brake_parking;
 
    // Landing Gear
    uint32_t gear_handle; // true=gear handle down; false= gear handle up
 
    // Switches
    uint32_t master_avionics;
 
        // nav and Comm
    double  comm_1;
    double  comm_2;
    double  nav_1;
    double  nav_2;
 
    // wind and turbulance
    double wind_speed_kt;
    double wind_dir_deg;
    double turbulence_norm;
 
    // temp and pressure
    double temp_c;
    double press_inhg;
 
    // other information about environment
    double hground;            // ground elevation (meters)
    double magvar;             // local magnetic variation in degs.
 
    // hazards
    uint32_t icing;                      // icing status could me much
                                         // more complex but I'm
                                         // starting simple here.
 
    // simulation control
    uint32_t speedup;            // integer speedup multiplier
    uint32_t freeze;             // 0=normal
                 // 0x01=master
                 // 0x02=position
                 // 0x04=fuel
 
    // --- New since FlightGear 0.9.10 (FG_NET_CTRLS_VERSION = 27)
 
    // --- Add new variables just before this line.
 
    uint32_t reserved[FG_NET_CTRLS_RESERVED_SPACE];  // 100 bytes reserved for future use.
};
 
 
#define FG_NET_FDM_VERSION 24
#define FG_NET_FDM_MAX_ENGINES 4
#define FG_NET_FDM_MAX_WHEELS  3
#define FG_NET_FDM_MAX_TANKS   4
 
#ifndef _NET_FDM_HXX
 
struct FGNetFDM {
 
  uint32_t version;           // increment when data values change
  uint32_t padding;           // padding
 
  // Positions
  double longitude;           // geodetic (radians)
  double latitude;            // geodetic (radians)
  double altitude;            // above sea level (meters)
  float agl;                  // above ground level (meters)
  float phi;                  // roll (radians)
  float theta;                // pitch (radians)
  float psi;                  // yaw or true heading (radians)
  float alpha;                // angle of attack (radians)
  float beta;                 // side slip angle (radians)
 
  // Velocities
  float phidot;               // roll rate (radians/sec)
  float thetadot;             // pitch rate (radians/sec)
  float psidot;               // yaw rate (radians/sec)
  float vcas;                 // calibrated airspeed
  float climb_rate;           // feet per second
  float v_north;              // north velocity in local/body frame, fps
  float v_east;               // east velocity in local/body frame, fps
  float v_down;               // down/vertical velocity in local/body frame, fps
  float v_body_u;             // ECEF velocity in body frame
  float v_body_v;             // ECEF velocity in body frame
  float v_body_w;             // ECEF velocity in body frame
 
  // Accelerations
  float A_X_pilot;            // X accel in body frame ft/sec^2
  float A_Y_pilot;            // Y accel in body frame ft/sec^2
  float A_Z_pilot;            // Z accel in body frame ft/sec^2
  // Stall
  float stall_warning;        // 0.0 - 1.0 indicating the amount of stall
  float slip_deg;             // slip ball deflection
 
  // Pressure
 
  // Engine status
  uint32_t num_engines;                       // Number of valid engines
  uint32_t eng_state[FG_NET_FDM_MAX_ENGINES]; // Engine state (off, cranking, running)
  float rpm[FG_NET_FDM_MAX_ENGINES];          // Engine RPM rev/min
  float fuel_flow[FG_NET_FDM_MAX_ENGINES];    // Fuel flow gallons/hr
  float fuel_px[FG_NET_FDM_MAX_ENGINES];      // Fuel pressure psi
  float egt[FG_NET_FDM_MAX_ENGINES];          // Exhuast gas temp deg F
  float cht[FG_NET_FDM_MAX_ENGINES];          // Cylinder head temp deg F
  float mp_osi[FG_NET_FDM_MAX_ENGINES];       // Manifold pressure
  float tit[FG_NET_FDM_MAX_ENGINES];          // Turbine Inlet Temperature
  float oil_temp[FG_NET_FDM_MAX_ENGINES];     // Oil temp deg F
  float oil_px[FG_NET_FDM_MAX_ENGINES];       // Oil pressure psi
 
  // Consumables
  uint32_t num_tanks;         // Max number of fuel tanks
  float fuel_quantity[FG_NET_FDM_MAX_TANKS];
 
  // Gear status
  uint32_t num_wheels;
  uint32_t wow[FG_NET_FDM_MAX_WHEELS];
  float gear_pos[FG_NET_FDM_MAX_WHEELS];
  float gear_steer[FG_NET_FDM_MAX_WHEELS];
  float gear_compression[FG_NET_FDM_MAX_WHEELS];
 
  // Environment
  uint32_t cur_time;           // current unix time
  // FIXME: make this uint64_t before 2038
  int32_t warp;                // offset in seconds to unix time
  float visibility;            // visibility in meters (for env. effects)
 
  // Control surface positions (normalized values)
  float elevator;
  float elevator_trim_tab;
  float left_flap;
  float right_flap;
  float left_aileron;
  float right_aileron;
  float rudder;
  float nose_wheel;
  float speedbrake;
  float spoilers;
};
 
#endif
 
struct FGNetMiniFDM {
   uint32_t version;           // increment when data values change
 
    // Positions
    double longitude;           // geodetic (radians)
    double latitude;            // geodetic (radians)
    double altitude;            // above sea level (meters)
    double agl;                 // above ground level (meters)
    double phi;                 // roll (radians)
    double theta;               // pitch (radians)
    double psi;                 // yaw or true heading (radians)
 
    // Velocities
    double vcas;
    double climb_rate;          // feet per second
 
    // Consumables
    uint32_t num_tanks;         // Max number of fuel tanks
    double fuel_quantity[FG_NET_FDM_MAX_TANKS];
 
    // Environment
    uint32_t cur_time;            // current unix time
    int32_t warp;                 // offset in seconds to unix time
};
 
#if FG_2_4
#define FG_NET_GUI_VERSION 7
#else
#define FG_NET_GUI_VERSION 8
#endif /*FG_2_4*/
 
#define FG_NET_GUI_MAX_TANKS 4
 
// Prior to FG_NET_GUI_VERSION 8, OS X needed #pragma pack(4) to
// properly display FG visualization data. In version 8 they added
// a padding1 element to ensure proper data alignment, so this is
// no longer required. The rest of this struct is based on FG source
// in src/Network/net_gui.hxx
 
#if FG_2_4
#ifdef __x86_64__
#pragma pack(push)
#ifdef __APPLE__
#pragma pack(4)
#else
#pragma pack(8)
#endif /*__APPLE__*/
#endif /*__x86_64__*/
#endif /*FG_2_4*/
struct FGNetGUI {
  uint32_t version;           // increment when data values change
  uint32_t padding1;
 
  // Positions
  double longitude;           // geodetic (radians)
  double latitude;            // geodetic (radians)
  float altitude;             // above sea level (meters)
  float agl;                  // above ground level (meters)
  float phi;                  // roll (radians)
  float theta;                // pitch (radians)
  float psi;                  // yaw or true heading (radians)
 
  // Velocities
  float vcas;
  float climb_rate;           // feet per second
 
  // Consumables
  uint32_t num_tanks;         // Max number of fuel tanks
  float fuel_quantity[FG_NET_GUI_MAX_TANKS];
 
  // Environment
  uint32_t cur_time;          // current unix time
                                // FIXME: make this uint64_t before 2038
  uint32_t warp;              // offset in seconds to unix time
  float ground_elev;          // ground elev (meters)
 
  // Approach
  float tuned_freq;           // currently tuned frequency
  float nav_radial;           // target nav radial
  uint32_t in_range;           // tuned navaid is in range?
  float dist_nm;              // distance to tuned navaid in nautical miles
  float course_deviation_deg; // degrees off target course
  float gs_deviation_deg;     // degrees off target glide slope
};
#if FG_2_4
#ifdef __x86_64__
#pragma pack(push)
#pragma pack(pop)
#endif /*__x86_64__*/
#endif /*FG_2_4*/
 
 
#define FG_ENVIRONMENT_FOOTER_MAGIC 0x12345678
// described in file fg_environment.xml (generic protocol)
struct FGEnvironment{
  double elapsed_sec;       // elapsed sim seconds
  float wind_from_north;    // wind from north in m/s
  float wind_from_east;     // wind from east in m/s
  float wind_from_down;     // wind from down in m/s
  float wind_from_heading;  // wind N-E heading in degrees
  float wind_speed;         // wind N-E speed in m/s
  uint32_t footer_magic;    // magic footer 0x12345678
};
 
 
 
extern void net_fdm_dump (struct FGNetFDM* fdm);
extern void net_fdm_ntoh (struct FGNetFDM* fdm);
extern void net_fdm_init (struct FGNetFDM* fdm);
 
extern void net_gui_init (struct FGNetGUI* gui);
extern void net_gui_hton (struct FGNetGUI* gui);
extern void net_gui_dump (struct FGNetGUI* gui);
 
extern void net_ctrls_dump(struct FGNetCtrls* ctrls);
extern void net_ctrls_ntoh(struct FGNetCtrls* ctrls);
 
#endif /* FLIGHT_GEAR_H */