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considering u,v,wbody-fps are the ECEF velocity expressed in body axis, change in all functions/variables name dealing with them, wrongly named with wind, or even north, east, down.

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This commit is contained in:
janodesbois 2013-10-22 15:34:23 +02:00
parent d127f7709f
commit ecfdf354f1
14 changed files with 79 additions and 79 deletions
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6
src/FDM/ExternalPipe/ExternalPipe.cxx
View file

@ -470,9 +470,9 @@ void FGExternalPipe::process_set_command( const string_list &tokens ) {
_set_Velocities_Local( net->v_north, _set_Velocities_Local( net->v_north,
net->v_east, net->v_east,
net->v_down ); net->v_down );
_set_Velocities_Wind_Body( net->v_wind_body_north, _set_Velocities_Body( net->v_body_u,
net->v_wind_body_east, net->v_body_v,
net->v_wind_body_down ); net->v_body_w );
_set_Accels_Pilot_Body( net->A_X_pilot, _set_Accels_Pilot_Body( net->A_X_pilot,
net->A_Y_pilot, net->A_Y_pilot,

12
src/FDM/JSBSim/JSBSim.cxx
View file

@ -760,9 +760,9 @@ bool FGJSBsim::copy_from_JSBsim()
Propagate->GetVel(FGJSBBase::eEast), Propagate->GetVel(FGJSBBase::eEast),
Propagate->GetVel(FGJSBBase::eDown) ); Propagate->GetVel(FGJSBBase::eDown) );
_set_Velocities_Wind_Body( Propagate->GetUVW(1), _set_Velocities_Body( Propagate->GetUVW(1),
Propagate->GetUVW(2), Propagate->GetUVW(2),
Propagate->GetUVW(3) ); Propagate->GetUVW(3) );
// Make the HUD work ... // Make the HUD work ...
_set_Velocities_Ground( Propagate->GetVel(FGJSBBase::eNorth), _set_Velocities_Ground( Propagate->GetVel(FGJSBBase::eNorth),
@ -1124,9 +1124,9 @@ void FGJSBsim::set_Velocities_Local( double north, double east, double down )
FGInterface::set_Velocities_Local(north, east, down); FGInterface::set_Velocities_Local(north, east, down);
} }
void FGJSBsim::set_Velocities_Wind_Body( double u, double v, double w) void FGJSBsim::set_Velocities_Body( double u, double v, double w)
{ {
SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Velocities_Wind_Body: " SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Velocities_Body: "
<< u << ", " << v << ", " << w ); << u << ", " << v << ", " << w );
if (needTrim) { if (needTrim) {
@ -1140,7 +1140,7 @@ void FGJSBsim::set_Velocities_Wind_Body( double u, double v, double w)
Propagate->SetUVW(3, w); Propagate->SetUVW(3, w);
} }
FGInterface::set_Velocities_Wind_Body(u, v, w); FGInterface::set_Velocities_Body(u, v, w);
} }
//Euler angles //Euler angles

2
src/FDM/JSBSim/JSBSim.hxx
View file

@ -166,7 +166,7 @@ public:
@param u X velocity in ft/sec @param u X velocity in ft/sec
@param v Y velocity in ft/sec @param v Y velocity in ft/sec
@param w Z velocity in ft/sec */ @param w Z velocity in ft/sec */
void set_Velocities_Wind_Body( double u, double v, double w); void set_Velocities_Body( double u, double v, double w);
//@} //@}
/** Euler Angle Parameter Set /** Euler Angle Parameter Set

6
src/FDM/LaRCsim/LaRCsim.cxx
View file

@ -653,7 +653,7 @@ bool FGLaRCsim::copy_from_LaRCsim() {
// set_Velocities_Local_Rel_Airmass( V_north_rel_airmass, // set_Velocities_Local_Rel_Airmass( V_north_rel_airmass,
// V_east_rel_airmass, V_down_rel_airmass ); // V_east_rel_airmass, V_down_rel_airmass );
// set_Velocities_Gust( U_gust, V_gust, W_gust ); // set_Velocities_Gust( U_gust, V_gust, W_gust );
_set_Velocities_Wind_Body( U_body, V_body, W_body ); _set_Velocities_Body( U_body, V_body, W_body );
_set_V_rel_wind( V_rel_wind ); _set_V_rel_wind( V_rel_wind );
// set_V_true_kts( V_true_kts ); // set_V_true_kts( V_true_kts );
@ -865,8 +865,8 @@ void FGLaRCsim::set_Velocities_Local( double north, double east, double down ){
copy_from_LaRCsim(); //update the bus copy_from_LaRCsim(); //update the bus
} }
void FGLaRCsim::set_Velocities_Wind_Body( double u, double v, double w){ void FGLaRCsim::set_Velocities_Body( double u, double v, double w){
SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Velocities_Wind_Body: " SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Velocities_Body: "
<< u << " " << v << " " << w ); << u << " " << v << " " << w );
snap_shot(); snap_shot();
lsic->SetUVWFpsIC(u,v,w); lsic->SetUVWFpsIC(u,v,w);

7
src/FDM/YASim/YASim.cxx
View file

@ -396,7 +396,7 @@ void YASim::copyToYASim(bool copyState)
// _set_Accels_CG_Body_N // _set_Accels_CG_Body_N
// _set_Velocities_Local // _set_Velocities_Local
// _set_Velocities_Ground // _set_Velocities_Ground
// _set_Velocities_Wind_Body // _set_Velocities_Body
// _set_Omega_Body // _set_Omega_Body
// _set_Euler_Rates // _set_Euler_Rates
// _set_Euler_Angles // _set_Euler_Angles
@ -469,6 +469,10 @@ void YASim::copyFromYASim()
// _set_Geocentric_Rates(M2FT*v[0], M2FT*v[1], M2FT*v[2]); // UNUSED // _set_Geocentric_Rates(M2FT*v[0], M2FT*v[1], M2FT*v[2]); // UNUSED
// ecef speed in body axis
Math::vmul33(s->orient, s->v, v);
_set_Velocities_Body(v[0]*M2FT, -v[1]*M2FT, -v[2]*M2FT);
// Airflow velocity. // Airflow velocity.
float wind[3]; float wind[3];
wind[0] = get_V_north_airmass() * FT2M * -1.0; // Wind in NED wind[0] = get_V_north_airmass() * FT2M * -1.0; // Wind in NED
@ -477,7 +481,6 @@ void YASim::copyFromYASim()
Math::tmul33(xyz2ned, wind, wind); // Wind in global Math::tmul33(xyz2ned, wind, wind); // Wind in global
Math::sub3(s->v, wind, v); // V - wind in global Math::sub3(s->v, wind, v); // V - wind in global
Math::vmul33(s->orient, v, v); // to body coordinates Math::vmul33(s->orient, v, v); // to body coordinates
_set_Velocities_Wind_Body(v[0]*M2FT, -v[1]*M2FT, -v[2]*M2FT);
_set_V_rel_wind(Math::mag3(v)*M2FT); // units? _set_V_rel_wind(Math::mag3(v)*M2FT); // units?
float P = _pressure_inhg->getFloatValue() * INHG2PA; float P = _pressure_inhg->getFloatValue() * INHG2PA;

16
src/FDM/flight.cxx
View file

@ -98,7 +98,7 @@ FGInterface::_setup ()
_state.v_local_v = SGVec3d::zeros(); _state.v_local_v = SGVec3d::zeros();
_state.v_local_rel_ground_v = SGVec3d::zeros(); _state.v_local_rel_ground_v = SGVec3d::zeros();
_state.v_local_airmass_v = SGVec3d::zeros(); _state.v_local_airmass_v = SGVec3d::zeros();
_state.v_wind_body_v = SGVec3d::zeros(); _state.v_body_v = SGVec3d::zeros();
_state.omega_body_v = SGVec3d::zeros(); _state.omega_body_v = SGVec3d::zeros();
_state.euler_rates_v = SGVec3d::zeros(); _state.euler_rates_v = SGVec3d::zeros();
_state.geocentric_rates_v = SGVec3d::zeros(); _state.geocentric_rates_v = SGVec3d::zeros();
@ -206,7 +206,7 @@ FGInterface::common_init ()
} else if ( speedset == "mach" || speedset == "MACH" ) { } else if ( speedset == "mach" || speedset == "MACH" ) {
set_Mach_number( fgGetDouble("/sim/presets/mach") ); set_Mach_number( fgGetDouble("/sim/presets/mach") );
} else if ( speedset == "UVW" || speedset == "uvw" ) { } else if ( speedset == "UVW" || speedset == "uvw" ) {
set_Velocities_Wind_Body( set_Velocities_Body(
fgGetDouble("/sim/presets/uBody-fps"), fgGetDouble("/sim/presets/uBody-fps"),
fgGetDouble("/sim/presets/vBody-fps"), fgGetDouble("/sim/presets/vBody-fps"),
fgGetDouble("/sim/presets/wBody-fps") ); fgGetDouble("/sim/presets/wBody-fps") );
@ -366,7 +366,7 @@ FGInterface::bind ()
_tiedProperties.Tie("/velocities/down-relground-fps", this, _tiedProperties.Tie("/velocities/down-relground-fps", this,
&FGInterface::get_V_down_rel_ground); // read-only &FGInterface::get_V_down_rel_ground); // read-only
// Relative wind // ECEF velocity in body axis
// FIXME: temporarily archivable, until the NED problem is fixed. // FIXME: temporarily archivable, until the NED problem is fixed.
_tiedProperties.Tie("/velocities/uBody-fps", this, _tiedProperties.Tie("/velocities/uBody-fps", this,
&FGInterface::get_uBody, &FGInterface::get_uBody,
@ -565,12 +565,12 @@ void FGInterface::set_Velocities_Local( double north,
_state.v_local_v[2] = down; _state.v_local_v[2] = down;
} }
void FGInterface::set_Velocities_Wind_Body( double u, void FGInterface::set_Velocities_Body( double u,
double v, double v,
double w){ double w){
_state.v_wind_body_v[0] = u; _state.v_body_v[0] = u;
_state.v_wind_body_v[1] = v; _state.v_body_v[1] = v;
_state.v_wind_body_v[2] = w; _state.v_body_v[2] = w;
} }
// Euler angles // Euler angles
@ -615,7 +615,7 @@ void FGInterface::_busdump(void)
SG_LOG(SG_FLIGHT,SG_INFO,"v_local_v: " << _state.v_local_v); SG_LOG(SG_FLIGHT,SG_INFO,"v_local_v: " << _state.v_local_v);
SG_LOG(SG_FLIGHT,SG_INFO,"v_local_rel_ground_v: " << _state.v_local_rel_ground_v); SG_LOG(SG_FLIGHT,SG_INFO,"v_local_rel_ground_v: " << _state.v_local_rel_ground_v);
SG_LOG(SG_FLIGHT,SG_INFO,"v_local_airmass_v: " << _state.v_local_airmass_v); SG_LOG(SG_FLIGHT,SG_INFO,"v_local_airmass_v: " << _state.v_local_airmass_v);
SG_LOG(SG_FLIGHT,SG_INFO,"v_wind_body_v: " << _state.v_wind_body_v); SG_LOG(SG_FLIGHT,SG_INFO,"v_body_v: " << _state.v_body_v);
SG_LOG(SG_FLIGHT,SG_INFO,"omega_body_v: " << _state.omega_body_v); SG_LOG(SG_FLIGHT,SG_INFO,"omega_body_v: " << _state.omega_body_v);
SG_LOG(SG_FLIGHT,SG_INFO,"euler_rates_v: " << _state.euler_rates_v); SG_LOG(SG_FLIGHT,SG_INFO,"euler_rates_v: " << _state.euler_rates_v);
SG_LOG(SG_FLIGHT,SG_INFO,"geocentric_rates_v: " << _state.geocentric_rates_v); SG_LOG(SG_FLIGHT,SG_INFO,"geocentric_rates_v: " << _state.geocentric_rates_v);

30
src/FDM/flight.hxx
View file

@ -162,7 +162,7 @@ private:
SGVec3d v_local_v; SGVec3d v_local_v;
SGVec3d v_local_rel_ground_v; // V rel w.r.t. earth surface SGVec3d v_local_rel_ground_v; // V rel w.r.t. earth surface
SGVec3d v_local_airmass_v; // velocity of airmass (steady winds) SGVec3d v_local_airmass_v; // velocity of airmass (steady winds)
SGVec3d v_wind_body_v; // Wind-relative velocities in body axis SGVec3d v_body_v; // ECEF velocities in body axis
SGVec3d omega_body_v; // Angular B rates SGVec3d omega_body_v; // Angular B rates
SGVec3d euler_rates_v; SGVec3d euler_rates_v;
@ -284,10 +284,10 @@ public:
_state.v_local_airmass_v[1] = east; _state.v_local_airmass_v[1] = east;
_state.v_local_airmass_v[2] = down; _state.v_local_airmass_v[2] = down;
} }
inline void _set_Velocities_Wind_Body( double u, double v, double w) { inline void _set_Velocities_Body( double u, double v, double w) {
_state.v_wind_body_v[0] = u; _state.v_body_v[0] = u;
_state.v_wind_body_v[1] = v; _state.v_body_v[1] = v;
_state.v_wind_body_v[2] = w; _state.v_body_v[2] = w;
} }
inline void _set_V_rel_wind(double vt) { _state.v_rel_wind = vt; } inline void _set_V_rel_wind(double vt) { _state.v_rel_wind = vt; }
inline void _set_V_ground_speed( double v) { _state.v_ground_speed = v; } inline void _set_V_ground_speed( double v) { _state.v_ground_speed = v; }
@ -456,15 +456,15 @@ public:
inline void set_V_down (double down) { inline void set_V_down (double down) {
set_Velocities_Local(_state.v_local_v[0], _state.v_local_v[1], down); set_Velocities_Local(_state.v_local_v[0], _state.v_local_v[1], down);
} }
virtual void set_Velocities_Wind_Body( double u, double v, double w); virtual void set_Velocities_Body( double u, double v, double w);
virtual void set_uBody (double uBody) { virtual void set_uBody (double uBody) {
set_Velocities_Wind_Body(uBody, _state.v_wind_body_v[1], _state.v_wind_body_v[2]); set_Velocities_Body(uBody, _state.v_body_v[1], _state.v_body_v[2]);
} }
virtual void set_vBody (double vBody) { virtual void set_vBody (double vBody) {
set_Velocities_Wind_Body(_state.v_wind_body_v[0], vBody, _state.v_wind_body_v[2]); set_Velocities_Body(_state.v_body_v[0], vBody, _state.v_body_v[2]);
} }
virtual void set_wBody (double wBody) { virtual void set_wBody (double wBody) {
set_Velocities_Wind_Body(_state.v_wind_body_v[0], _state.v_wind_body_v[1], wBody); set_Velocities_Body(_state.v_body_v[0], _state.v_body_v[1], wBody);
} }
// Euler angles // Euler angles
@ -538,9 +538,9 @@ public:
inline double get_V_north() const { return _state.v_local_v[0]; } inline double get_V_north() const { return _state.v_local_v[0]; }
inline double get_V_east() const { return _state.v_local_v[1]; } inline double get_V_east() const { return _state.v_local_v[1]; }
inline double get_V_down() const { return _state.v_local_v[2]; } inline double get_V_down() const { return _state.v_local_v[2]; }
inline double get_uBody () const { return _state.v_wind_body_v[0]; } inline double get_uBody () const { return _state.v_body_v[0]; }
inline double get_vBody () const { return _state.v_wind_body_v[1]; } inline double get_vBody () const { return _state.v_body_v[1]; }
inline double get_wBody () const { return _state.v_wind_body_v[2]; } inline double get_wBody () const { return _state.v_body_v[2]; }
// Please dont comment these out. fdm=ada uses these (see // Please dont comment these out. fdm=ada uses these (see
// cockpit.cxx) ---> // cockpit.cxx) --->
@ -559,9 +559,9 @@ public:
inline double get_V_east_airmass() const { return _state.v_local_airmass_v[1]; } inline double get_V_east_airmass() const { return _state.v_local_airmass_v[1]; }
inline double get_V_down_airmass() const { return _state.v_local_airmass_v[2]; } inline double get_V_down_airmass() const { return _state.v_local_airmass_v[2]; }
inline double get_U_body() const { return _state.v_wind_body_v[0]; } inline double get_U_body() const { return _state.v_body_v[0]; }
inline double get_V_body() const { return _state.v_wind_body_v[1]; } inline double get_V_body() const { return _state.v_body_v[1]; }
inline double get_W_body() const { return _state.v_wind_body_v[2]; } inline double get_W_body() const { return _state.v_body_v[2]; }
inline double get_V_rel_wind() const { return _state.v_rel_wind; } inline double get_V_rel_wind() const { return _state.v_rel_wind; }

6
src/FDM/flightProperties.cxx
View file

@ -266,10 +266,10 @@ void FlightProperties::set_Velocities_Local(double x, double y, double z)
_root->setDoubleValue("velocities/speed-down-fps", z); _root->setDoubleValue("velocities/speed-down-fps", z);
} }
void FlightProperties::set_Velocities_Wind_Body(double x, double y, double z) void FlightProperties::set_Velocities_Body(double x, double y, double z)
{ {
_root->setDoubleValue("velocities/vBody-fps", x); _root->setDoubleValue("velocities/uBody-fps", x);
_root->setDoubleValue("velocities/uBody-fps", y); _root->setDoubleValue("velocities/vBody-fps", y);
_root->setDoubleValue("velocities/wBody-fps", z); _root->setDoubleValue("velocities/wBody-fps", z);
} }

2
src/FDM/flightProperties.hxx
View file

@ -119,7 +119,7 @@ public:
void set_Climb_Rate(double fps); void set_Climb_Rate(double fps);
void set_Velocities_Local(double x, double y, double z); void set_Velocities_Local(double x, double y, double z);
void set_Velocities_Wind_Body(double x, double y, double z); void set_Velocities_Body(double x, double y, double z);
void set_Accels_Pilot_Body(double x, double y, double z); void set_Accels_Pilot_Body(double x, double y, double z);
private: private:
SGPropertyNode* _root; SGPropertyNode* _root;

24
src/Network/native_fdm.cxx
View file

@ -151,9 +151,9 @@ void FGProps2NetFDM( FGNetFDM *net, bool net_byte_order ) {
net->v_north = fdm_state.get_V_north(); net->v_north = fdm_state.get_V_north();
net->v_east = fdm_state.get_V_east(); net->v_east = fdm_state.get_V_east();
net->v_down = fdm_state.get_V_down(); net->v_down = fdm_state.get_V_down();
net->v_wind_body_north = fdm_state.get_uBody(); net->v_body_u = fdm_state.get_uBody();
net->v_wind_body_east = fdm_state.get_vBody(); net->v_body_v = fdm_state.get_vBody();
net->v_wind_body_down = fdm_state.get_wBody(); net->v_body_w = fdm_state.get_wBody();
net->A_X_pilot = fdm_state.get_A_X_pilot(); net->A_X_pilot = fdm_state.get_A_X_pilot();
net->A_Y_pilot = fdm_state.get_A_Y_pilot(); net->A_Y_pilot = fdm_state.get_A_Y_pilot();
@ -245,9 +245,9 @@ void FGProps2NetFDM( FGNetFDM *net, bool net_byte_order ) {
htonf(net->v_north); htonf(net->v_north);
htonf(net->v_east); htonf(net->v_east);
htonf(net->v_down); htonf(net->v_down);
htonf(net->v_wind_body_north); htonf(net->v_body_u);
htonf(net->v_wind_body_east); htonf(net->v_body_v);
htonf(net->v_wind_body_down); htonf(net->v_body_w);
htonf(net->A_X_pilot); htonf(net->A_X_pilot);
htonf(net->A_Y_pilot); htonf(net->A_Y_pilot);
@ -327,9 +327,9 @@ void FGNetFDM2Props( FGNetFDM *net, bool net_byte_order ) {
htonf(net->v_north); htonf(net->v_north);
htonf(net->v_east); htonf(net->v_east);
htonf(net->v_down); htonf(net->v_down);
htonf(net->v_wind_body_north); htonf(net->v_body_u);
htonf(net->v_wind_body_east); htonf(net->v_body_v);
htonf(net->v_wind_body_down); htonf(net->v_body_w);
htonf(net->A_X_pilot); htonf(net->A_X_pilot);
htonf(net->A_Y_pilot); htonf(net->A_Y_pilot);
@ -410,9 +410,9 @@ void FGNetFDM2Props( FGNetFDM *net, bool net_byte_order ) {
fdm_state.set_Velocities_Local( net->v_north, fdm_state.set_Velocities_Local( net->v_north,
net->v_east, net->v_east,
net->v_down ); net->v_down );
fdm_state.set_Velocities_Wind_Body( net->v_wind_body_north, fdm_state.set_Velocities_Body( net->v_body_u,
net->v_wind_body_east, net->v_body_v,
net->v_wind_body_down ); net->v_body_w );
fdm_state.set_Accels_Pilot_Body( net->A_X_pilot, fdm_state.set_Accels_Pilot_Body( net->A_X_pilot,
net->A_Y_pilot, net->A_Y_pilot,

9
src/Network/net_fdm.hxx
View file

@ -61,12 +61,9 @@ public:
float v_north; // north velocity in local/body frame, fps float v_north; // north velocity in local/body frame, fps
float v_east; // east 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_down; // down/vertical velocity in local/body frame, fps
float v_wind_body_north; // north velocity in local/body frame float v_body_u; // ECEF velocity in body frame
// relative to local airmass, fps float v_body_v; // ECEF velocity in body frame
float v_wind_body_east; // east velocity in local/body frame float v_body_w; // ECEF velocity in body frame
// relative to local airmass, fps
float v_wind_body_down; // down/vertical velocity in local/body
// frame relative to local airmass, fps
// Accelerations // Accelerations
float A_X_pilot; // X accel in body frame ft/sec^2 float A_X_pilot; // X accel in body frame ft/sec^2

12
utils/GPSsmooth/MIDG_main.cxx
View file

@ -148,9 +148,9 @@ static void midg2fg( const MIDGpos pos, const MIDGatt att,
fdm->v_north = 0.0; fdm->v_north = 0.0;
fdm->v_east = 0.0; fdm->v_east = 0.0;
fdm->v_down = 0.0; fdm->v_down = 0.0;
fdm->v_wind_body_north = 0.0; fdm->v_body_u = 0.0;
fdm->v_wind_body_east = 0.0; fdm->v_body_v = 0.0;
fdm->v_wind_body_down = 0.0; fdm->v_body_w = 0.0;
fdm->stall_warning = 0.0; fdm->stall_warning = 0.0;
fdm->A_X_pilot = 0.0; fdm->A_X_pilot = 0.0;
@ -224,9 +224,9 @@ static void midg2fg( const MIDGpos pos, const MIDGatt att,
htonf(fdm->v_north); htonf(fdm->v_north);
htonf(fdm->v_east); htonf(fdm->v_east);
htonf(fdm->v_down); htonf(fdm->v_down);
htonf(fdm->v_wind_body_north); htonf(fdm->v_body_u);
htonf(fdm->v_wind_body_east); htonf(fdm->v_body_v);
htonf(fdm->v_wind_body_down); htonf(fdm->v_body_w);
htonf(fdm->A_X_pilot); htonf(fdm->A_X_pilot);
htonf(fdm->A_Y_pilot); htonf(fdm->A_Y_pilot);

12
utils/GPSsmooth/UGear_main.cxx
View file

@ -210,9 +210,9 @@ static void ugear2fg( gps *gpspacket, imu *imupacket, nav *navpacket,
fdm->v_north = 0.0; fdm->v_north = 0.0;
fdm->v_east = 0.0; fdm->v_east = 0.0;
fdm->v_down = 0.0; fdm->v_down = 0.0;
fdm->v_wind_body_north = 0.0; fdm->v_body_u = 0.0;
fdm->v_wind_body_east = 0.0; fdm->v_body_v = 0.0;
fdm->v_wind_body_down = 0.0; fdm->v_body_w = 0.0;
fdm->stall_warning = 0.0; fdm->stall_warning = 0.0;
fdm->A_X_pilot = 0.0; fdm->A_X_pilot = 0.0;
@ -301,9 +301,9 @@ static void ugear2fg( gps *gpspacket, imu *imupacket, nav *navpacket,
htonf(fdm->v_north); htonf(fdm->v_north);
htonf(fdm->v_east); htonf(fdm->v_east);
htonf(fdm->v_down); htonf(fdm->v_down);
htonf(fdm->v_wind_body_north); htonf(fdm->v_body_u);
htonf(fdm->v_wind_body_east); htonf(fdm->v_body_v);
htonf(fdm->v_wind_body_down); htonf(fdm->v_body_w);
htonf(fdm->A_X_pilot); htonf(fdm->A_X_pilot);
htonf(fdm->A_Y_pilot); htonf(fdm->A_Y_pilot);

12
utils/GPSsmooth/gps_main.cxx
View file

@ -150,9 +150,9 @@ static void gps2fg( const GPSPoint p, FGNetFDM *fdm, FGNetCtrls *ctrls )
fdm->v_north = 0.0; fdm->v_north = 0.0;
fdm->v_east = 0.0; fdm->v_east = 0.0;
fdm->v_down = 0.0; fdm->v_down = 0.0;
fdm->v_wind_body_north = 0.0; fdm->v_body_u = 0.0;
fdm->v_wind_body_east = 0.0; fdm->v_body_v = 0.0;
fdm->v_wind_body_down = 0.0; fdm->v_body_w = 0.0;
fdm->stall_warning = 0.0; fdm->stall_warning = 0.0;
fdm->A_X_pilot = 0.0; fdm->A_X_pilot = 0.0;
@ -226,9 +226,9 @@ static void gps2fg( const GPSPoint p, FGNetFDM *fdm, FGNetCtrls *ctrls )
htonf(fdm->v_north); htonf(fdm->v_north);
htonf(fdm->v_east); htonf(fdm->v_east);
htonf(fdm->v_down); htonf(fdm->v_down);
htonf(fdm->v_wind_body_north); htonf(fdm->v_body_u);
htonf(fdm->v_wind_body_east); htonf(fdm->v_body_v);
htonf(fdm->v_wind_body_down); htonf(fdm->v_body_w);
htonf(fdm->A_X_pilot); htonf(fdm->A_X_pilot);
htonf(fdm->A_Y_pilot); htonf(fdm->A_Y_pilot);