X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FFDM%2FBalloon.cxx;h=dd5bc016d8f8580432532adc857e9bcbb6daa138;hb=938d006188e70e891bc04e91610c7b8caaca87b6;hp=44afb4f4e121c4c72df5d431ec1472a7d11df0cd;hpb=12168687cb764047b4d47ce2e87e2a2374e2ceb0;p=flightgear.git diff --git a/src/FDM/Balloon.cxx b/src/FDM/Balloon.cxx index 44afb4f4e..dd5bc016d 100644 --- a/src/FDM/Balloon.cxx +++ b/src/FDM/Balloon.cxx @@ -39,7 +39,7 @@ HISTORY #include -#ifdef FG_MATH_EXCEPTION_CLASH +#ifdef SG_MATH_EXCEPTION_CLASH # include #endif @@ -47,12 +47,13 @@ HISTORY #include #include -#include -#include +#include +#include #include #include -#include
+#include
+#include
#include "Balloon.h" @@ -61,23 +62,36 @@ HISTORY /****************************************************************************/ +FGBalloonSim::FGBalloonSim( double dt ) { + //set the dt of the model + current_balloon.set_dt(dt); +} + + +FGBalloonSim::~FGBalloonSim() { +} + + // Initialize the BalloonSim flight model, dt is the time increment for // each subsequent iteration through the EOM -int FGBalloonSim::init( double dt ) { - sgVec3 temp; +void FGBalloonSim::init() { + + //do init common to all the FDM's + common_init(); + + //now do init specific to the Balloon - FG_LOG( FG_FLIGHT, FG_INFO, "Starting initializing BalloonSim" ); + sgVec3 temp; - FG_LOG( FG_FLIGHT, FG_INFO, " created a balloon" ); + SG_LOG( SG_FLIGHT, SG_INFO, "Starting initializing BalloonSim" ); - //set the dt of the model - current_balloon.set_dt(dt); + SG_LOG( SG_FLIGHT, SG_INFO, " created a balloon" ); //set position sgSetVec3( temp, get_Latitude(), get_Longitude(), - get_Altitude() * FEET_TO_METER); + get_Altitude() * SG_FEET_TO_METER); current_balloon.setPosition( temp ); //set Euler angles (?) @@ -89,19 +103,17 @@ int FGBalloonSim::init( double dt ) { //set velocities sgSetVec3( temp, - current_options.get_uBody(), - current_options.get_vBody(), - current_options.get_wBody() ); + fgGetDouble("/velocities/uBody-fps"), + fgGetDouble("/velocities/vBody-fps"), + fgGetDouble("/velocities/wBody-fps") ); current_balloon.setVelocity( temp ); - FG_LOG( FG_FLIGHT, FG_INFO, "Finished initializing BalloonSim" ); - - return 1; + SG_LOG( SG_FLIGHT, SG_INFO, "Finished initializing BalloonSim" ); } // Run an iteration of the EOM (equations of motion) -int FGBalloonSim::update( int multiloop ) { +void FGBalloonSim::update( int multiloop ) { double save_alt = 0.0; // lets try to avoid really screwing up the BalloonSim model @@ -111,11 +123,11 @@ int FGBalloonSim::update( int multiloop ) { } // set control positions - current_balloon.set_burner_strength ( controls.get_throttle(0) ); + current_balloon.set_burner_strength ( globals->get_controls()->get_throttle(0) ); //not more implemented yet // Inform BalloonSim of the local terrain altitude - current_balloon.setGroundLevel ( get_Runway_altitude() * FEET_TO_METER); + current_balloon.setGroundLevel ( get_Runway_altitude() * SG_FEET_TO_METER); // old -- FGInterface_2_JSBsim() not needed except for Init() // translate FG to JSBsim structure @@ -140,7 +152,7 @@ int FGBalloonSim::update( int multiloop ) { /*sgVec3 temp, temp2; current_balloon.getPosition( temp ); current_balloon.getVelocity( temp2 ); - FG_LOG( FG_FLIGHT, FG_INFO, "T: " << current_balloon.getTemperature() << + SG_LOG( SG_FLIGHT, SG_INFO, "T: " << current_balloon.getTemperature() << " alt: " << temp[2] << " gr_alt: " << get_Runway_altitude() << " burner: " << controls.get_elevator() << @@ -150,70 +162,40 @@ int FGBalloonSim::update( int multiloop ) { if ( save_alt < -9000.0 ) { set_Altitude( save_alt ); } - - return 1; } // Convert from the FGInterface struct to the BalloonSim -int FGBalloonSim::copy_to_BalloonSim() { - return 1; +bool FGBalloonSim::copy_to_BalloonSim() { + return true; } // Convert from the BalloonSim to the FGInterface struct -int FGBalloonSim::copy_from_BalloonSim() { +bool FGBalloonSim::copy_from_BalloonSim() { sgVec3 temp; // Velocities current_balloon.getVelocity( temp ); - set_Velocities_Local( temp[0], temp[1], temp[2] ); + _set_Velocities_Local( temp[0], temp[1], temp[2] ); - /* ***FIXME*** */ set_V_equiv_kts( sgLengthVec3 ( temp ) ); + /* ***FIXME*** */ _set_V_equiv_kts( sgLengthVec3 ( temp ) ); - set_Omega_Body( 0.0, 0.0, 0.0 ); + _set_Omega_Body( 0.0, 0.0, 0.0 ); // Positions current_balloon.getPosition( temp ); - double lat_geoc = temp[0]; - double lon = temp[1]; - double alt = temp[2] * METER_TO_FEET; - - double lat_geod, tmp_alt, sl_radius1, sl_radius2, tmp_lat_geoc; - fgGeocToGeod( lat_geoc, EQUATORIAL_RADIUS_M + alt * FEET_TO_METER, - &lat_geod, &tmp_alt, &sl_radius1 ); - fgGeodToGeoc( lat_geod, alt * FEET_TO_METER, &sl_radius2, &tmp_lat_geoc ); - - FG_LOG( FG_FLIGHT, FG_DEBUG, "lon = " << lon << " lat_geod = " << lat_geod - << " lat_geoc = " << lat_geoc - << " alt = " << alt << " tmp_alt = " << tmp_alt * METER_TO_FEET - << " sl_radius1 = " << sl_radius1 * METER_TO_FEET - << " sl_radius2 = " << sl_radius2 * METER_TO_FEET - << " Equator = " << EQUATORIAL_RADIUS_FT ); - - set_Geocentric_Position( lat_geoc, lon, - sl_radius2 * METER_TO_FEET + alt ); - set_Geodetic_Position( lat_geod, lon, alt ); + //temp[0]: geocentric latitude + //temp[1]: longitude + //temp[2]: altitude (meters) + _updateGeocentricPosition( temp[0], temp[1], temp[2] * SG_METER_TO_FEET ); + current_balloon.getHPR( temp ); set_Euler_Angles( temp[0], temp[1], temp[2] ); - set_Euler_Rates(0,0,0); - - set_Alpha( 0.0/*FDMExec.GetTranslation()->Getalpha()*/ ); - set_Beta( 0.0/*FDMExec.GetTranslation()->Getbeta()*/ ); - - /* **FIXME*** */ set_Sea_level_radius( sl_radius2 * METER_TO_FEET ); - /* **FIXME*** */ set_Earth_position_angle( 0.0 ); - - /* ***FIXME*** */ set_Runway_altitude( 0.0 ); - - set_sin_lat_geocentric( lat_geoc ); - set_cos_lat_geocentric( lat_geoc ); - set_sin_cos_longitude( lon ); - set_sin_cos_latitude( lat_geod ); - - return 0; + + return true; }