-#include <simgear/misc/sg_path.hxx>
#include <simgear/debug/logstream.hxx>
+#include <simgear/misc/sg_path.hxx>
+#include <simgear/scene/model/location.hxx>
+#include <simgear/scene/model/placement.hxx>
#include <simgear/xml/easyxml.hxx>
+
#include <Main/globals.hxx>
#include <Main/fg_props.hxx>
+#include <Model/acmodel.hxx>
#include "FGFDM.hpp"
#include "Atmosphere.hpp"
using namespace yasim;
-static const float RAD2DEG = 180/3.14159265358979323846;
+static const float YASIM_PI = 3.14159265358979323846;
+static const float RAD2DEG = 180/YASIM_PI;
+static const float PI2 = YASIM_PI*2;
static const float RAD2RPM = 9.54929658551;
static const float M2FT = 3.2808399;
static const float FT2M = 0.3048;
// fgGetFloat("/engines/engine[0]/epr"),
// fgGetFloat("/engines/engine[0]/egt"));
-// printf("gear: %f\n", fgGetFloat("/controls/gear-down"));
+// printf("gear: %f\n", fgGetFloat("/controls/gear/gear-down"));
// printf("alpha %5.1f beta %5.1f\n", get_Alpha()*57.3, get_Beta()*57.3);
float cg[3];
char buf[256];
a->getModel()->getBody()->getCG(cg);
- sprintf(buf, " CG: %.1f, %.1f, %.1f", cg[0], cg[1], cg[2]);
+ sprintf(buf, " CG: %.3f, %.3f, %.3f", cg[0], cg[1], cg[2]);
SG_LOG(SG_FLIGHT, SG_INFO, buf);
if(a->getFailureMsg()) {
// Superclass hook
common_init();
-
m->setCrashed(false);
+ // Figure out the initial speed type
+ string speed_set = fgGetString("/sim/presets/speed-set", "UVW");
+ if (speed_set == "NED")
+ _speed_set = NED;
+ else if (speed_set == "UVW")
+ _speed_set = UVW;
+ else if (speed_set == "knots")
+ _speed_set = KNOTS;
+ else if (speed_set == "mach")
+ _speed_set = MACH;
+ else {
+ _speed_set = UVW;
+ SG_LOG(SG_FLIGHT, SG_ALERT, "Unknown speed type " << speed_set);
+ }
+
// Build a filename and parse it
- SGPath f(globals->get_fg_root());
- f.append("Aircraft-yasim");
+ SGPath f(fgGetString("/sim/aircraft-dir"));
f.append(fgGetString("/sim/aero"));
f.concat(".xml");
readXML(f.str(), *_fdm);
node->setDoubleValue("yoffset-in", pos[1]);
node->setDoubleValue("zoffset-in", pos[2]);
}
- for(i=0; i<m->numThrusters(); i++) {
- // Sanify the initial input conditions
- char buf[64];
- sprintf(buf, "/controls/throttle[%d]", i); fgSetFloat(buf, 0);
- sprintf(buf, "/controls/mixture[%d]", i); fgSetFloat(buf, 1);
- sprintf(buf, "/controls/propeller-pitch[%d]", i); fgSetFloat(buf, 1);
- sprintf(buf, "/controls/afterburner[%d]", i); fgSetFloat(buf, 0);
- }
-
- fgSetFloat("/controls/slats", 0);
- fgSetFloat("/controls/spoilers", 0);
+// for(i=0; i<m->numThrusters(); i++) {
+// // Sanify the initial input conditions
+// char buf[64];
+// sprintf(buf, "/controls/engines/engine[%d]/throttle", i); fgSetFloat(buf, 0);
+// sprintf(buf, "/controls/engines/engine[%d]/mixture", i); fgSetFloat(buf, 1);
+// sprintf(buf, "/controls/engines/engine[%d]/propeller-pitch", i); fgSetFloat(buf, 1);
+// sprintf(buf, "/controls/engines/engine[%d]/augmentation", i); fgSetFloat(buf, 0);
+// }
+
+// fgSetFloat("/controls/flight/slats", 0);
+// fgSetFloat("/controls/flight/spoilers", 0);
// Are we at ground level? If so, lift the plane up so the gear
// clear the ground.
double runway_altitude = get_Runway_altitude();
- fgSetBool("/controls/gear-down", false);
if(get_Altitude() - runway_altitude < 50) {
+ fgSetBool("/controls/gear/gear-down", false);
float minGearZ = 1e18;
for(i=0; i<a->numGear(); i++) {
Gear* g = a->getGear(i);
minGearZ = pos[2];
}
_set_Altitude(runway_altitude - minGearZ*M2FT);
- fgSetBool("/controls/gear-down", true);
+ fgSetBool("/controls/gear/gear-down", true);
}
// The pilot's eyepoint
wind[2] = get_V_down_airmass() * FT2M * -1.0;
// Get ground elevation from the FGinterface's FGlocation data
- double ground = getACModel()->get3DModel()->getFGLocation()->get_cur_elev_m();
+ double ground = getACModel()->get3DModel()->getSGLocation()->get_cur_elev_m();
// cout << "YASIM: ground = " << ground << endl;
float pressure = fgGetFloat("/environment/pressure-inhg") * INHG2PA;
Glue::euler2orient(roll, pitch, hdg, s.orient);
Math::mmul33(s.orient, xyz2ned, s.orient);
- // Copy in the existing velocity for now...
- Math::set3(model->getState()->v, s.v);
+ // Velocity
+ string speed_set = fgGetString("/sim/presets/speed-set", "UVW");
+ float v[3];
+ bool needCopy = false;
+ switch (_speed_set) {
+ case NED:
+ v[0] = get_V_north() * FT2M * -1.0;
+ v[1] = get_V_east() * FT2M * -1.0;
+ v[2] = get_V_down() * FT2M * -1.0;
+ break;
+ case UVW:
+ v[0] = get_uBody() * FT2M;
+ v[1] = get_vBody() * FT2M;
+ v[2] = get_wBody() * FT2M;
+ Math::tmul33(s.orient, v, v);
+ break;
+ case KNOTS:
+ v[0] = Atmosphere::spdFromVCAS(get_V_calibrated_kts()/MPS2KTS,
+ pressure, temp);
+ v[1] = 0;
+ v[2] = 0;
+ Math::tmul33(s.orient, v, v);
+ needCopy = true;
+ break;
+ case MACH:
+ v[0] = Atmosphere::spdFromMach(get_Mach_number(), temp);
+ v[1] = 0;
+ v[2] = 0;
+ Math::tmul33(s.orient, v, v);
+ needCopy = true;
+ break;
+ default:
+ v[0] = 0;
+ v[1] = 0;
+ v[2] = 0;
+ break;
+ }
+ if (!copyState)
+ _speed_set = UVW; // change to this after initial setting
+ Math::set3(v, s.v);
- if(copyState)
+ if(copyState || needCopy)
model->setState(&s);
// wind
wind[2] = get_V_down_airmass() * FT2M * -1.0;
Math::tmul33(xyz2ned, wind, wind); // Wind in global
Math::sub3(s->v, wind, v); // V - wind in global
- Math::vmul33(s->orient, s->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_Accels_CG_Body(M2FT*v[0], -M2FT*v[1], -M2FT*v[2]);
_fdm->getAirplane()->getPilotAccel(v);
- _set_Accels_Pilot_Body(M2FT*v[0], M2FT*v[1], -M2FT*v[2]);
+ _set_Accels_Pilot_Body(-M2FT*v[0], M2FT*v[1], M2FT*v[2]);
+
+ // There is no property for pilot G's, but I need it for a panel
+ // instrument. Hack this in here, and REMOVE IT WHEN IT FINDS A
+ // REAL HOME!
+ fgSetFloat("/accelerations/pilot-g", -v[2]/9.8);
// The one appears (!) to want inverted pilot acceleration
// numbers, in G's...
Math::mmul33(s->orient, tmp, tmp);
float roll, pitch, hdg;
Glue::orient2euler(tmp, &roll, &pitch, &hdg);
+ // make heading positive value
+ if(hdg < 0.0) hdg += PI2;
_set_Euler_Angles(roll, pitch, hdg);
// rotation
node->setBoolValue("running", t->isRunning());
node->setBoolValue("cranking", t->isCranking());
- // Note: assumes all tanks have the same fuel density!
- node->setDoubleValue("fuel-flow-gph", CM2GALS * t->getFuelFlow()
- / airplane->getFuelDensity(0));
-
float tmp[3];
t->getThrust(tmp);
node->setDoubleValue("prop-thrust", Math::mag3(tmp) * KG2LBS / 9.8);
projects / flightgear.git / blobdiff