// Set SRB class specs
void Atlantis_SRB::clbkSetClassCaps (FILEHANDLE cfg)
{
extern PARTICLESTREAMSPEC srb_contrail, srb_exhaust;
PARTICLESTREAMSPEC srb_bolt = {
0, 8.0, 20, 0.0, 0.1, 0.3, 16, 3.0, PARTICLESTREAMSPEC::EMISSIVE,
PARTICLESTREAMSPEC::LVL_LIN, 0, 1,
PARTICLESTREAMSPEC::ATM_FLAT, 1, 1
};
SetEnableFocus (false);
// SRB cannot receive input focus
// *********************** physical parameters *********************************
SetSize (23.0);
SetEmptyMass (SRB_EMPTY_MASS);
SetCW (0.1, 0.3, 1.4, 1.4);
SetCrossSections (_V(162.1,162.1,26.6));
SetRotDrag (_V(0.7,0.7,0.1));
SetPMI (_V(154.3,154.3,1.83));
//SetGravityGradientDamping (10.0);
SetTouchdownPoints (tdvtx, ntdvtx);
SetLiftCoeffFunc (0);
// ************************* docking port **************************************
CreateDock (_V(1.95,0,5),_V(1,0,0),_V(0,0,1)); // ET attachment
// ************************* propellant specs **********************************
ph_main = CreatePropellantResource (SRB_MAX_PROPELLANT_MASS);
// *********************** thruster definitions ********************************
// main engine
th_main = CreateThruster (_V(0,0,-21), THRUSTGIMBAL_LAUNCH, SRB_THRUST_MAX, ph_main, SRB_ISP0, SRB_ISP1);
SURFHANDLE tex = oapiRegisterExhaustTexture ("Exhaust2");
srb_exhaust.tex = oapiRegisterParticleTexture ("Contrail2");
AddExhaust (th_main, 16.0, 2.0, tex);
AddExhaustStream (th_main, _V(0,0,-30), &srb_contrail);
AddExhaustStream (th_main, _V(0,0,-25), &srb_exhaust);
// separation bolts
th_bolt = CreateThruster (_V(0,0,3.0), _V(-1,0,0), 3e6, ph_main, 1e7);
// for simplicity, the separation bolts directly use SRB propellant. We give
// them an insanely high ISP to avoid significant propellant drainage
AddExhaust (th_bolt, 0.7, 0.1, _V(2.1,0,-8), _V(-1,0,0));
AddExhaust (th_bolt, 0.7, 0.1, _V(2.1,0,11), _V(-1,0,0));
AddExhaustStream (th_bolt, _V(2.1,0,0), &srb_bolt);
// ************************ visual parameters **********************************
AddMesh (hSRBMesh);
bMainEngine = false;
bSeparationEngine = false;
bGimbalCmd = false;
srbpos = SRB_UNDEFINED;
}
void Sat5Abort2::init()
{
SetSize (15);
SetCOG_elev (15.225);
SetEmptyMass (233000);
SetMaxFuelMass (471000);
SetFuelMass(444760);
//SetISP (ISP_SECOND_VAC);
SetISP (4780);
//slThrust = CalcSeaLevelThrust(THRUST_SECOND_VAC,ISP_SECOND_VAC,ISP_SECOND_SL, 106000);
//vacThrust = THRUST_SECOND_VAC;
//vessel->SetMaxThrust (ENGINE_MAIN, slThrust);
SetMaxThrust (ENGINE_MAIN, 6008625);
SetMaxThrust (ENGINE_RETRO, 0);
SetMaxThrust (ENGINE_HOVER, 0);
SetMaxThrust (ENGINE_ATTITUDE, 5e4);
SetEngineLevel(ENGINE_MAIN, 0.0);
SetPMI (_V(374,374,80));
SetCrossSections (_V(524,524,97));
SetCW (0.1, 0.3, 1.4, 1.4);
SetRotDrag (_V(0.7,0.7,1.2));
SetPitchMomentScale (0);
SetBankMomentScale (0);
SetLiftCoeffFunc (0);
ClearMeshes();
ClearExhaustRefs();
ClearAttExhaustRefs();
//vessel->ShiftCentreOfMass (_V(0,0,12.25));
VECTOR3 mesh_dir=_V(0,0,-17.2-STG1O);
AddMesh (hsat5stg2, &mesh_dir);
mesh_dir=_V(0,0,2.-STG1O);
AddMesh (hsat5stg3, &mesh_dir);
mesh_dir=_V(-1.48,-1.48,14.55-STG1O);
AddMesh (hsat5stg31, &mesh_dir);
mesh_dir=_V(1.48,-1.48,14.55-STG1O);
AddMesh (hsat5stg32, &mesh_dir);
mesh_dir=_V(1.48,1.48,14.55-STG1O);
AddMesh (hsat5stg33, &mesh_dir);
mesh_dir=_V(-1.48,1.48,14.55-STG1O);
AddMesh (hsat5stg34, &mesh_dir);
mesh_dir=_V(0,SMVO,19.1-STG1O);
AddMesh (hSM, &mesh_dir);
VECTOR3 m_exhaust_ref = {0,0,-1};
VECTOR3 m_exhaust_pos1= {0,0,-28.25-STG1O};
VECTOR3 m_exhaust_pos2= {2,2,-28.25-STG1O};
VECTOR3 m_exhaust_pos3= {-2,2,-28.25-STG1O};
VECTOR3 m_exhaust_pos4 = {2,-2.0,-28.25-STG1O};
VECTOR3 m_exhaust_pos5 = {-2,-2,-28.25-STG1O};
AddExhaustRef (EXHAUST_MAIN, m_exhaust_pos1, 25.0, 1.5, &m_exhaust_ref);
AddExhaustRef (EXHAUST_MAIN, m_exhaust_pos2, 25.0, 1.5, &m_exhaust_ref);
AddExhaustRef (EXHAUST_MAIN, m_exhaust_pos3, 25.0, 1.5, &m_exhaust_ref);
AddExhaustRef (EXHAUST_MAIN, m_exhaust_pos4, 25.0, 1.5, &m_exhaust_ref);
AddExhaustRef (EXHAUST_MAIN, m_exhaust_pos5, 25.0, 1.5, &m_exhaust_ref);
status = 3;
SetCameraOffset (_V(-1,1.0,32.4-STG1O));
}
void EVA::init ()
{
GoDock1 = false;
SetSize (3.5);
SetEmptyMass (115);
SetMaxFuelMass (10);
SetFuelMass (10);
SetISP(10000);
SetMaxThrust (ENGINE_ATTITUDE, 5);
SetEngineLevel(ENGINE_MAIN, 0.0);
SetPMI (_V(5,5,5));
SetRotDrag (_V(0.7,0.7,1.2));
SetPitchMomentScale (0);
SetBankMomentScale (0);
SetLiftCoeffFunc (0);
ClearMeshes();
ClearExhaustRefs();
ClearAttExhaustRefs();
VECTOR3 mesh_dir=_V(0,0,0);
AddMesh (hCMPEVA, &mesh_dir);
}
// --------------------------------------------------------------
// Set the capabilities of the vessel class
// --------------------------------------------------------------
void SolarSail::clbkSetClassCaps (FILEHANDLE cfg)
{
// physical specs
SetSize (SAIL_RADIUS*2.0);
SetEmptyMass (100.0);
SetCW (0.3, 0.3, 0.6, 0.9);
SetWingAspect (0.7);
SetWingEffectiveness (2.5);
SetCrossSections (_V(10.5,15.0,5.8));
SetRotDrag (_V(0.6,0.6,0.35));
if (GetFlightModel() >= 1) {
SetPitchMomentScale (1e-4);
SetYawMomentScale (1e-4);
}
SetPMI (_V(3e3,3e3,6e3));
SetTrimScale (0.05);
SetCameraOffset (_V(0,0.8,0));
SetLiftCoeffFunc (LiftCoeff);
SetDockParams (_V(0,1.3,-1), _V(0,1,0), _V(0,0,-1));
SetTouchdownPoints (_V(0,-1.5,2), _V(-1,-1.5,-1.5), _V(1,-1.5,-1.5));
// visual specs
AddMesh (hMeshTpl);
}
// --------------------------------------------------------------
// Set the capabilities of the vessel class
// --------------------------------------------------------------
void ShuttlePB::clbkSetClassCaps (FILEHANDLE cfg)
{
THRUSTER_HANDLE th_main, th_hover, th_rcs[14], th_group[4];
// physical vessel parameters
SetSize (PB_SIZE);
SetEmptyMass (PB_EMPTYMASS);
SetPMI (PB_PMI);
SetCrossSections (PB_CS);
SetRotDrag (PB_RD);
SetTouchdownPoints (PB_TDP[0], PB_TDP[1], PB_TDP[2]);
// docking port definitions
SetDockParams (PB_DOCK_POS, PB_DOCK_DIR, PB_DOCK_ROT);
// airfoil definitions
CreateAirfoil3 (LIFT_VERTICAL, PB_COP, vlift, NULL, PB_VLIFT_C, PB_VLIFT_S, PB_VLIFT_A);
CreateAirfoil3 (LIFT_HORIZONTAL, PB_COP, hlift, NULL, PB_HLIFT_C, PB_HLIFT_S, PB_HLIFT_A);
// control surface animations
UINT anim_Laileron = CreateAnimation (0.5);
UINT anim_Raileron = CreateAnimation (0.5);
UINT anim_elevator = CreateAnimation (0.5);
AddAnimationComponent (anim_Laileron, 0, 1, &trans_Laileron);
AddAnimationComponent (anim_Raileron, 0, 1, &trans_Raileron);
AddAnimationComponent (anim_elevator, 0, 1, &trans_Lelevator);
AddAnimationComponent (anim_elevator, 0, 1, &trans_Relevator);
// aerodynamic control surface defintions
CreateControlSurface (AIRCTRL_ELEVATOR, 1.5, 0.7, _V( 0,0,-2.5), AIRCTRL_AXIS_XPOS, anim_elevator);
CreateControlSurface (AIRCTRL_AILERON, 1.5, 0.25, _V( 1,0,-2.5), AIRCTRL_AXIS_XPOS, anim_Laileron);
CreateControlSurface (AIRCTRL_AILERON, 1.5, 0.25, _V(-1,0,-2.5), AIRCTRL_AXIS_XNEG, anim_Raileron);
// propellant resources
PROPELLANT_HANDLE hpr = CreatePropellantResource (PB_FUELMASS);
// main engine
th_main = CreateThruster (_V(0,0,-4.35), _V(0,0,1), PB_MAXMAINTH, hpr, PB_ISP);
CreateThrusterGroup (&th_main, 1, THGROUP_MAIN);
AddExhaust (th_main, 8, 1, _V(0,0.3,-4.35), _V(0,0,-1));
PARTICLESTREAMSPEC contrail_main = {
0, 5.0, 16, 200, 0.15, 1.0, 5, 3.0, PARTICLESTREAMSPEC::DIFFUSE,
PARTICLESTREAMSPEC::LVL_PSQRT, 0, 2,
PARTICLESTREAMSPEC::ATM_PLOG, 1e-4, 1
};
PARTICLESTREAMSPEC exhaust_main = {
0, 2.0, 20, 200, 0.05, 0.1, 8, 1.0, PARTICLESTREAMSPEC::EMISSIVE,
PARTICLESTREAMSPEC::LVL_SQRT, 0, 1,
PARTICLESTREAMSPEC::ATM_PLOG, 1e-5, 0.1
};
AddExhaustStream (th_main, _V(0,0.3,-10), &contrail_main);
AddExhaustStream (th_main, _V(0,0.3,-5), &exhaust_main);
// hover engine
th_hover = CreateThruster (_V(0,-1.5,0), _V(0,1,0), PB_MAXHOVERTH, hpr, PB_ISP);
CreateThrusterGroup (&th_hover, 1, THGROUP_HOVER);
AddExhaust (th_hover, 8, 1, _V(0,-1.5,1), _V(0,-1,0));
AddExhaust (th_hover, 8, 1, _V(0,-1.5,-1), _V(0,-1,0));
PARTICLESTREAMSPEC contrail_hover = {
0, 5.0, 8, 200, 0.15, 1.0, 5, 3.0, PARTICLESTREAMSPEC::DIFFUSE,
PARTICLESTREAMSPEC::LVL_PSQRT, 0, 2,
PARTICLESTREAMSPEC::ATM_PLOG, 1e-4, 1
};
PARTICLESTREAMSPEC exhaust_hover = {
0, 2.0, 10, 200, 0.05, 0.05, 8, 1.0, PARTICLESTREAMSPEC::EMISSIVE,
PARTICLESTREAMSPEC::LVL_SQRT, 0, 1,
PARTICLESTREAMSPEC::ATM_PLOG, 1e-5, 0.1
};
AddExhaustStream (th_hover, _V(0,-3, 1), &contrail_hover);
AddExhaustStream (th_hover, _V(0,-3,-1), &contrail_hover);
AddExhaustStream (th_hover, _V(0,-2, 1), &exhaust_hover);
AddExhaustStream (th_hover, _V(0,-2,-1), &exhaust_hover);
// RCS engines
th_rcs[ 0] = CreateThruster (_V( 1,0, 3), _V(0, 1,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[ 1] = CreateThruster (_V( 1,0, 3), _V(0,-1,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[ 2] = CreateThruster (_V(-1,0, 3), _V(0, 1,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[ 3] = CreateThruster (_V(-1,0, 3), _V(0,-1,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[ 4] = CreateThruster (_V( 1,0,-3), _V(0, 1,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[ 5] = CreateThruster (_V( 1,0,-3), _V(0,-1,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[ 6] = CreateThruster (_V(-1,0,-3), _V(0, 1,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[ 7] = CreateThruster (_V(-1,0,-3), _V(0,-1,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[ 8] = CreateThruster (_V( 1,0, 3), _V(-1,0,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[ 9] = CreateThruster (_V(-1,0, 3), _V( 1,0,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[10] = CreateThruster (_V( 1,0,-3), _V(-1,0,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[11] = CreateThruster (_V(-1,0,-3), _V( 1,0,0), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[12] = CreateThruster (_V( 0,0,-3), _V(0,0, 1), PB_MAXRCSTH, hpr, PB_ISP);
th_rcs[13] = CreateThruster (_V( 0,0, 3), _V(0,0,-1), PB_MAXRCSTH, hpr, PB_ISP);
th_group[0] = th_rcs[0];
th_group[1] = th_rcs[2];
th_group[2] = th_rcs[5];
th_group[3] = th_rcs[7];
CreateThrusterGroup (th_group, 4, THGROUP_ATT_PITCHUP);
th_group[0] = th_rcs[1];
th_group[1] = th_rcs[3];
th_group[2] = th_rcs[4];
th_group[3] = th_rcs[6];
CreateThrusterGroup (th_group, 4, THGROUP_ATT_PITCHDOWN);
th_group[0] = th_rcs[0];
th_group[1] = th_rcs[4];
th_group[2] = th_rcs[3];
th_group[3] = th_rcs[7];
CreateThrusterGroup (th_group, 4, THGROUP_ATT_BANKLEFT);
th_group[0] = th_rcs[1];
th_group[1] = th_rcs[5];
th_group[2] = th_rcs[2];
th_group[3] = th_rcs[6];
CreateThrusterGroup (th_group, 4, THGROUP_ATT_BANKRIGHT);
th_group[0] = th_rcs[0];
th_group[1] = th_rcs[4];
th_group[2] = th_rcs[2];
th_group[3] = th_rcs[6];
CreateThrusterGroup (th_group, 4, THGROUP_ATT_UP);
th_group[0] = th_rcs[1];
th_group[1] = th_rcs[5];
th_group[2] = th_rcs[3];
th_group[3] = th_rcs[7];
CreateThrusterGroup (th_group, 4, THGROUP_ATT_DOWN);
th_group[0] = th_rcs[8];
th_group[1] = th_rcs[11];
CreateThrusterGroup (th_group, 2, THGROUP_ATT_YAWLEFT);
th_group[0] = th_rcs[9];
th_group[1] = th_rcs[10];
CreateThrusterGroup (th_group, 2, THGROUP_ATT_YAWRIGHT);
th_group[0] = th_rcs[8];
th_group[1] = th_rcs[10];
CreateThrusterGroup (th_group, 2, THGROUP_ATT_LEFT);
th_group[0] = th_rcs[9];
th_group[1] = th_rcs[11];
CreateThrusterGroup (th_group, 2, THGROUP_ATT_RIGHT);
CreateThrusterGroup (th_rcs+12, 1, THGROUP_ATT_FORWARD);
CreateThrusterGroup (th_rcs+13, 1, THGROUP_ATT_BACK);
// camera parameters
SetCameraOffset (_V(0,0.8,0));
// associate a mesh for the visual
AddMesh ("ShuttlePB");
}
void LEM::SetLmAscentHoverStage()
{
ClearThrusterDefinitions();
agc.SetVesselStats(APS_ISP, APS_THRUST, true);
ShiftCentreOfMass(_V(0.0,3.0,0.0));
SetSize (5);
SetCOG_elev (5);
SetEmptyMass (1920.0);
SetPMI(_V(2.8, 2.29, 2.37));
SetCrossSections (_V(21,23,17));
SetCW (0.1, 0.3, 1.4, 1.4);
SetRotDrag (_V(0.7,0.7,0.7));
SetPitchMomentScale (0);
SetBankMomentScale (0);
SetLiftCoeffFunc (0);
ClearMeshes();
ClearExhaustRefs();
ClearAttExhaustRefs();
double tdph = -5.8;
SetTouchdownPoints (_V(0, tdph, 5), _V(-5, tdph, -5), _V(5, tdph, -5));
VSSetTouchdownPoints(GetHandle(), _V(0, tdph, 5), _V(-5, tdph, -5), _V(5, tdph, -5));
VECTOR3 mesh_dir=_V(-0.191,-0.02,+0.383);
UINT meshidx = AddMesh (hLMAscent, &mesh_dir);
SetMeshVisibilityMode (meshidx, MESHVIS_VCEXTERNAL);
if (!ph_Asc)
ph_Asc = CreatePropellantResource(AscentFuelMassKg); // 2nd stage Propellant
SetDefaultPropellantResource (ph_Asc); // Display 2nd stage propellant level in generic HUD
// orbiter main thrusters
th_hover[0] = CreateThruster (_V( 0.0, -2.5, 0.0), _V( 0,1,0), APS_THRUST, ph_Asc, APS_ISP);
th_hover[1] = CreateThruster (_V( 0.01, -2.0, 0.0), _V( 0,1,0), 0, ph_Asc, 0); // this is a "virtual engine",no thrust and no fuel
// needed for visual gimbaling for corrected engine flames
DelThrusterGroup(THGROUP_HOVER,true);
thg_hover = CreateThrusterGroup (th_hover, 2, THGROUP_HOVER);
AddExhaust (th_hover[1], 6.0, 0.8, exhaustTex);
SetCameraOffset (_V(-1,1.0,0.0));
status = 2;
stage = 2;
SetEngineLevel(ENGINE_HOVER,0);
AddRCS_LMH2(-1.86);
bModeHover=true;
if(ph_Dsc){
DelPropellantResource(ph_Dsc);
ph_Dsc = 0;
}
VECTOR3 dockpos = {0.0 ,0.58, 0.0};
VECTOR3 dockdir = {0,1,0};
VECTOR3 dockrot = { -0.8660254, 0, 0.5 };
SetDockParams(dockpos, dockdir, dockrot);
hattDROGUE = CreateAttachment(true, dockpos, dockdir, dockrot, "PADROGUE");
InitNavRadios (4);
LDGswitch=false;
AFEED1switch=true;
AFEED2switch=true;
AFEED3switch=true;
AFEED4switch=true;
// Descent stage detached.
agc.SetInputChannelBit(030, DescendStageAttached, false);
CheckRCS();
}
void LEM::SetLmVesselHoverStage()
{
ClearThrusterDefinitions();
agc.SetVesselStats(DPS_ISP, DPS_THRUST, true);
SetEmptyMass(AscentFuelMassKg + 4374.0);
SetSize (7);
SetPMI (_V(3.26,2.22,3.26));
SetCrossSections (_V(24.53,21.92,24.40));
// SetPMI (_V(2.8,2.29,2.37));
// SetCrossSections (_V(21,23,17));
SetCW (0.1, 0.3, 1.4, 1.4);
SetRotDrag (_V(0.7,0.7,0.7));
SetPitchMomentScale (0);
SetBankMomentScale (0);
SetLiftCoeffFunc (0);
ClearMeshes();
ClearExhaustRefs();
ClearAttExhaustRefs();
SetTouchdownPoints (_V(0, -3.86, 5), _V(-5, -3.86, -5), _V(5, -3.86, -5));
VSSetTouchdownPoints(GetHandle(), _V(0, -3.86, 5), _V(-5, -3.86, -5), _V(5, -3.86, -5));
VECTOR3 mesh_dir=_V(-0.003,-0.03,0.004);
UINT meshidx;
if (Landed) {
meshidx = AddMesh (hLMLanded, &mesh_dir);
}else{
UINT probeidx;
meshidx = AddMesh (hLMLanded, &mesh_dir);
probeidx = AddMesh (hLemProbes, &mesh_dir);
SetMeshVisibilityMode (probeidx, MESHVIS_VCEXTERNAL);
}
SetMeshVisibilityMode (meshidx, MESHVIS_VCEXTERNAL);
if (!ph_Dsc){
ph_Dsc = CreatePropellantResource(DescentFuelMassKg); //2nd stage Propellant
}
SetDefaultPropellantResource (ph_Dsc); // display 2nd stage propellant level in generic HUD
if (!ph_RCSA){
ph_RCSA = CreatePropellantResource(133.084001);
}
if (!ph_RCSB){
ph_RCSB = CreatePropellantResource(133.084001);
}
// orbiter main thrusters
th_hover[0] = CreateThruster (_V(0.0 , -2.0, 0.0), _V(0,1,0), 46706.3, ph_Dsc, 3107);
th_hover[1] = CreateThruster (_V(0.013, -2.8, -0.034), _V(0,1,0), 0, ph_Dsc, 0); //this is a "virtual engine",no thrust and no fuel
//needed for visual gimbaling for corrected engine flames
DelThrusterGroup(THGROUP_HOVER,true);
thg_hover = CreateThrusterGroup(th_hover, 2, THGROUP_HOVER);
AddExhaust (th_hover[1], 10.0, 1.5, exhaustTex);
SetCameraOffset (_V(-1,1.0,0.0));
status = 1;
stage = 1;
SetEngineLevel(ENGINE_HOVER,0);
AddRCS_LMH(-1.85);
bModeHover=true;
VECTOR3 dockpos = {0.0 ,2.6, 0.0};
VECTOR3 dockdir = {0,1,0};
VECTOR3 dockrot = { -0.8660254, 0, 0.5 };
SetDockParams(dockpos, dockdir, dockrot);
hattDROGUE = CreateAttachment(true, dockpos, dockdir, dockrot, "PADROGUE");
InitNavRadios (4);
LDGswitch=true;
ATT2switch=true;
ATT3switch=true;
ATT1switch=true;
AFEED1switch=false;
AFEED2switch=false;
AFEED3switch=false;
AFEED4switch=false;
// Descent stage attached.
agc.SetInputChannelBit(030, DescendStageAttached, true);
CheckRCS();
}
void LEM::SetLmVesselDockStage()
{
double fuelmass;
int mnumber;
ClearThrusterDefinitions();
agc.SetVesselStats(DPS_ISP, DPS_THRUST, true);
//
// Changed to reflect mission-specific empty and fuel mass
//
// From "Apollo by the Numbers"
//
mnumber=agc.GetApolloNo();
if(mnumber < 15) {
SetEmptyMass(6565);
fuelmass=8375.;
} else {
SetEmptyMass(7334);
fuelmass=8891.;
}
SetSize (6);
// SetPMI (_V(2.8,2.29,2.37));
SetPMI(_V(2.5428, 2.2871, 2.7566));
// SetCrossSections (_V(21,23,17));
//SetPMI(_V(3.26, 2.22, 3.26));
SetCrossSections (_V(24.53,21.92,24.40));
SetCW (0.1, 0.3, 1.4, 1.4);
SetRotDrag (_V(0.7,0.7,0.7));
SetPitchMomentScale (0);
SetBankMomentScale (0);
SetLiftCoeffFunc (0);
ClearMeshes();
ClearExhaustRefs();
ClearAttExhaustRefs();
SetTouchdownPoints (_V(0,0,10), _V(-1,0,-10), _V(1,0,-10));
VECTOR3 mesh_dir=_V(0.0,-0.2,0.03);
UINT meshidx = AddMesh (hLMPKD, &mesh_dir);
SetMeshVisibilityMode (meshidx, MESHVIS_VCEXTERNAL);
if (!ph_Dsc)
ph_Dsc = CreatePropellantResource(fuelmass); //2nd stage Propellant
SetDefaultPropellantResource (ph_Dsc); // display 2nd stage propellant level in generic HUD
// 133.084001 kg is 293.4 pounds, which is the fuel + oxidizer capacity of one RCS tank.
if (!ph_RCSA) {
ph_RCSA = CreatePropellantResource(133.084001);
}
if (!ph_RCSB) {
ph_RCSB = CreatePropellantResource(133.084001);
}
// orbiter main thrusters
th_hover[0] = CreateThruster (_V(0.0 , -3.3, 0.0), _V(0,1,0), 46706.3, ph_Dsc, 3107);
th_hover[1] = CreateThruster (_V(0.013, -3.0, -0.03), _V(0,1,0), 0, ph_Dsc, 0); //this is a "virtual engine",no thrust and no fuel
//needed for visual gimbaling for corrected engine flames
DelThrusterGroup(THGROUP_HOVER,true);
thg_hover = CreateThrusterGroup(th_hover, 2, THGROUP_HOVER);
AddExhaust(th_hover[1], 10.0, 1.2, exhaustTex);
SetCameraOffset (_V(-1,1.0,0.0));
SetEngineLevel(ENGINE_HOVER,0);
AddRCS_LMH(-1.85);
status = 0;
stage = 0;
bModeDocked=true;
VECTOR3 dockpos = {0.0 ,2.6, 0.0};
VECTOR3 dockdir = {0,1,0};
VECTOR3 dockrot = { -0.8660254, 0, 0.5 };
SetDockParams(dockpos, dockdir, dockrot);
hattDROGUE = CreateAttachment(true, dockpos, dockdir, dockrot, "PADROGUE");
InitNavRadios (4);
LDGswitch=false;
ATT2switch=true;
ATT3switch=true;
ATT1switch=true;
AFEED1switch=false;
AFEED2switch=false;
AFEED3switch=false;
AFEED4switch=false;
// Descent stage attached.
agc.SetInputChannelBit(030, DescendStageAttached, true);
CheckRCS();
}