DLLCLBK VESSEL *ovcInit (OBJHANDLE hvessel, int flightmodel)
{
if (!refcount++)
{
hCMPEVA = oapiLoadMeshGlobal ("ProjectApollo/saturn1_CMP_EVA");
}
return new EVA (hvessel, flightmodel);
}
void LEMLoadMeshes()
{
hLMPKD = oapiLoadMeshGlobal ("ProjectApollo/LM_NoWheel");
hLMLanded = oapiLoadMeshGlobal ("ProjectApollo/LM_Landed");
hLMDescent = oapiLoadMeshGlobal ("ProjectApollo/LM_descent");
hLMAscent = oapiLoadMeshGlobal ("ProjectApollo/LM_ascent");
hLMAscent2= oapiLoadMeshGlobal ("ProjectApollo/LM_ascent2");
hAstro1= oapiLoadMeshGlobal ("ProjectApollo/Sat5AstroS");
hLemProbes = oapiLoadMeshGlobal ("ProjectApollo/LM_ContactProbes");
}
DLLCLBK VESSEL *ovcInit (OBJHANDLE hvessel, int flightmodel)
{
if (!refcount++) {
hSat1stg1 = oapiLoadMeshGlobal ("ProjectApollo/nsat1stg1");
hSat1stg2 = oapiLoadMeshGlobal ("ProjectApollo/nsat1stg2");
hSat1stg21 = oapiLoadMeshGlobal ("ProjectApollo/nsat1stg21");
hSat1stg22 = oapiLoadMeshGlobal ("ProjectApollo/nsat1stg22");
hSat1stg23 = oapiLoadMeshGlobal ("ProjectApollo/nsat1stg23");
hSat1stg24 = oapiLoadMeshGlobal ("ProjectApollo/nsat1stg24");
hSM = oapiLoadMeshGlobal ("ProjectApollo/SM");
}
return new VESSEL (hvessel, flightmodel);
}
void InterplanetarySC::clbkSetClassCaps(FILEHANDLE cfg)
{
MESHHANDLE mesh;
mesh = oapiLoadMeshGlobal("ThermalFissionCraft");
UINT idx;
idx = AddMesh(mesh);
SetMeshVisibilityMode(idx,MESHVIS_EXTERNAL);
SetSize(350.0);
SetEmptyMass(400000.0);
createSubSystems();
}
DLLCLBK VESSEL *ovcInit (OBJHANDLE hvessel, int flightmodel)
{
if (!refcount++) {
hsat5stg2 = oapiLoadMeshGlobal ("ProjectApollo/sat5stg2");
hsat5stg3 = oapiLoadMeshGlobal ("ProjectApollo/sat5stg3");
hsat5stg31 = oapiLoadMeshGlobal ("ProjectApollo/sat5stg31");
hsat5stg32 = oapiLoadMeshGlobal ("ProjectApollo/sat5stg32");
hsat5stg33 = oapiLoadMeshGlobal ("ProjectApollo/sat5stg33");
hsat5stg34 = oapiLoadMeshGlobal ("ProjectApollo/sat5stg34");
hSM = oapiLoadMeshGlobal ("ProjectApollo/SM");
}
return new Sat5Abort2 (hvessel, flightmodel);
}
// Set vessel class parameters
void Dragonfly::SetClassCaps (FILEHANDLE cfg)
{
int i;
SetSize (4.0);
SetEmptyMass (EMPTY_MASS);
SetCrossSections (_V(23.7,22.5,17.3));
SetPMI (_V(5.4,5.4,2.5));
SetCameraOffset (_V(0,1.5,0));
// ************************* propellant specs **********************************
ph_main = CreatePropellantResource (MAX_MAIN_FUEL);
// *********************** thruster definitions ********************************
// thrusters in left pod
th_lp[0] = CreateThruster (_V(-3.5,0,0), _V(1,0,0), 2*MAX_RCS_THRUST, ph_main, ISP);
th_lp[1] = CreateThruster (_V(-2.98,0,-0.8), _V(0,0,1), MAX_RCS_THRUST, ph_main, ISP);
th_lp[2] = CreateThruster (_V(-2.98,0,0.8), _V(0,0,-1), MAX_RCS_THRUST, ph_main, ISP);
th_lp[3] = CreateThruster (_V(-2.98,-0.8,0), _V(0,1,0), MAX_RCS_THRUST, ph_main, ISP);
th_lp[4] = CreateThruster (_V(-2.98,0.8,0), _V(0,-1,0), MAX_RCS_THRUST, ph_main, ISP);
// thrusters in right pod
th_rp[0] = CreateThruster (_V(3.5,0,0), _V(-1,0,0), 2*MAX_RCS_THRUST, ph_main, ISP);
th_rp[1] = CreateThruster (_V(2.98,0,-0.8), _V(0,0,1), MAX_RCS_THRUST, ph_main, ISP);
th_rp[2] = CreateThruster (_V(2.98,0,0.8), _V(0,0,-1), MAX_RCS_THRUST, ph_main, ISP);
th_rp[3] = CreateThruster (_V(2.98,-0.8,0), _V(0,1,0), MAX_RCS_THRUST, ph_main, ISP);
th_rp[4] = CreateThruster (_V(2.98,0.8,0), _V(0,-1,0), MAX_RCS_THRUST, ph_main, ISP);
// thrusters in aft pod (rotational RCS)
th_ap[0] = CreateThruster (_V(-0.8,0,-11.1), _V(1,0,0), MAX_RCS_THRUST, ph_main, ISP);
th_ap[1] = CreateThruster (_V(0.8,0,-11.1), _V(-1,0,0), MAX_RCS_THRUST, ph_main, ISP);
th_ap[2] = CreateThruster (_V(0,-0.8,-11.1), _V(0,1,0), MAX_RCS_THRUST, ph_main, ISP);
th_ap[3] = CreateThruster (_V(0,0.8,-11.1), _V(0,-1,0), MAX_RCS_THRUST, ph_main, ISP);
// exhaust definitions for left pod
AddExhaust (th_lp[0], 1, 0.15, _V(-3.5,0.18,-0.18), _V(-1,0,0));
AddExhaust (th_lp[0], 1, 0.15, _V(-3.5,-0.18,0.18), _V(-1,0,0));
for (i = 1; i < 5; i++) AddExhaust (th_lp[i], 1, 0.15);
// exhaust definitions for right pod
AddExhaust (th_rp[0], 1, 0.15, _V(3.5,-0.18,-0.18), _V(1,0,0));
AddExhaust (th_rp[0], 1, 0.15, _V(3.5,0.18,0.18), _V(1,0,0));
for (i = 1; i < 5; i++) AddExhaust (th_rp[i], 1, 0.15);
// exhaust definitions for aft pod
for (i = 0; i < 4; i++) AddExhaust (th_ap[i], 1, 0.15);
//thruster definitions. Both manual and "automatic" RCS
SetManualRCS();
SetNormalRCS();//
// *************************** docking port ************************************
SetDockParams (_V(0,0,3.2), _V(0,0,1), _V(0,1,0));
// ******************************** mesh ***************************************
AddMesh (oapiLoadMeshGlobal ("Dragonfly"));
};
// --------------------------------------------------------------
// One-time global setup across all instances
// --------------------------------------------------------------
void SolarSail::GlobalSetup()
{
SolarSail::hMeshTpl = oapiLoadMeshGlobal ("SolarSail");
oapiSetMeshProperty (SolarSail::hMeshTpl, MESHPROPERTY_MODULATEMATALPHA, 1);
SetupElasticity (hMeshTpl);
}
// Constructor
Atlantis_SRB::Atlantis_SRB (OBJHANDLE hObj)
: VESSEL2(hObj)
{
// preload mesh
hSRBMesh = oapiLoadMeshGlobal ("Atlantis_srb");
}