void Dragonfly::SetManualRCS() {//we define manual RCS groups // thruster group definitions th[0] = th_lp[0]; th_lin_right=CreateThrusterGroup (th, 1, THGROUP_USER); // need to add counter-balance in aft pod th[0] = th_rp[0]; th_lin_left=CreateThrusterGroup (th, 1, THGROUP_USER); th[0] = th_lp[3]; th[1] = th_rp[3]; th_lin_up=CreateThrusterGroup (th, 2, THGROUP_USER); th[0] = th_lp[4]; th[1] = th_rp[4]; th_lin_down=CreateThrusterGroup (th, 2, THGROUP_USER); th[0] = th_lp[1]; th[1] = th_rp[1]; th_lin_forward=CreateThrusterGroup (th, 2, THGROUP_USER); th[0] = th_lp[2]; th[1] = th_rp[2]; th_lin_back=CreateThrusterGroup (th, 2, THGROUP_USER); th[0] = th_lp[3]; th[1] = th_rp[4]; th_rot_rlrgt=CreateThrusterGroup (th, 2, THGROUP_USER); th[0] = th_lp[4]; th[1] = th_rp[3]; th_rot_rllft=CreateThrusterGroup (th, 2, THGROUP_USER); th_rot_left=CreateThrusterGroup (th_ap+0, 1, THGROUP_USER); th_rot_right=CreateThrusterGroup (th_ap+1, 1, THGROUP_USER); th_rot_down=CreateThrusterGroup (th_ap+2, 1, THGROUP_USER); th_rot_up=CreateThrusterGroup (th_ap+3, 1, THGROUP_USER); }
void Dragonfly::SetNormalRCS() { DeleteAutoRCS(); //??need to delete them again? SetZeroManualRCS(); //just in case // thruster group definitions (or re-definition) th[0] = th_lp[0]; CreateThrusterGroup (th, 1, THGROUP_ATT_RIGHT); // need to add counter-balance in aft pod th[0] = th_rp[0]; CreateThrusterGroup (th, 1, THGROUP_ATT_LEFT); th[0] = th_lp[3]; th[1] = th_rp[3]; CreateThrusterGroup (th, 2, THGROUP_ATT_UP); th[0] = th_lp[4]; th[1] = th_rp[4]; CreateThrusterGroup (th, 2, THGROUP_ATT_DOWN); th[0] = th_lp[1]; th[1] = th_rp[1]; CreateThrusterGroup (th, 2, THGROUP_ATT_FORWARD); th[0] = th_lp[2]; th[1] = th_rp[2]; CreateThrusterGroup (th, 2, THGROUP_ATT_BACK); th[0] = th_lp[3]; th[1] = th_rp[4]; CreateThrusterGroup (th, 2, THGROUP_ATT_BANKRIGHT); th[0] = th_lp[4]; th[1] = th_rp[3]; CreateThrusterGroup (th, 2, THGROUP_ATT_BANKLEFT); CreateThrusterGroup (th_ap+0, 1, THGROUP_ATT_YAWLEFT); CreateThrusterGroup (th_ap+1, 1, THGROUP_ATT_YAWRIGHT); CreateThrusterGroup (th_ap+2, 1, THGROUP_ATT_PITCHDOWN); CreateThrusterGroup (th_ap+3, 1, THGROUP_ATT_PITCHUP); Manual_RCS=0;//we've gone to Auto };
// -------------------------------------------------------------- // 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(); }