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synced 2024-12-23 08:10:01 +00:00
helis done + cheats
This commit is contained in:
parent
7ddfc40675
commit
ae8deff131
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@ -291,6 +291,38 @@ void KangarooCheat()
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}
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}
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#endif
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#endif
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#ifdef ALLCARSHELI_CHEAT
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void AllCarsHeliCheat(void)
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{
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wchar* string;
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if (bAllCarCheat) {
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string = TheText.Get("CHEATOF");
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bAllCarCheat = false;
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}
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else {
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string = TheText.Get("CHEAT1");
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bAllCarCheat = true;
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}
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CHud::SetHelpMessage(string, true);
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}
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#endif
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#ifdef ALT_DODO_CHEAT
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void AltDodoCheat(void)
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{
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wchar* string;
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if (CVehicle::bAltDodoCheat) {
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string = TheText.Get("CHEATOF");
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CVehicle::bAltDodoCheat = false;
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}
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else {
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string = TheText.Get("CHEAT1");
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CVehicle::bAltDodoCheat = true;
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}
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CHud::SetHelpMessage(string, true);
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}
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#endif
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void
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void
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CControllerState::Clear(void)
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CControllerState::Clear(void)
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{
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{
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@ -862,6 +894,18 @@ void CPad::AddToPCCheatString(char c)
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CPed::SwitchDebugDisplay();
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CPed::SwitchDebugDisplay();
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#endif
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#endif
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#ifdef ALLCARSHELI_CHEAT
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// "CARSAREHELI"
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if (!_CHEATCMP("ILEHERASRAC"))
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AllCarsHeliCheat();
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#endif
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#ifdef ALT_DODO_CHEAT
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// "IWANTTOMASTERDODO"
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if (!_CHEATCMP("ODODRETSAMOTTNAWI"))
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AltDodoCheat();
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#endif
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#undef _CHEATCMP
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#undef _CHEATCMP
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}
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}
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@ -450,3 +450,7 @@ public:
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VALIDATE_SIZE(CPad, 0xFC);
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VALIDATE_SIZE(CPad, 0xFC);
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extern CPad Pads[MAX_PADS];
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extern CPad Pads[MAX_PADS];
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#ifdef ALLCARSHELI_CHEAT
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extern bool bAllCarCheat;
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#endif
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@ -202,6 +202,8 @@ enum Config {
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// Pad
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// Pad
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#define XINPUT
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#define XINPUT
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#define KANGAROO_CHEAT
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#define KANGAROO_CHEAT
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#define ALLCARSHELI_CHEAT
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#define ALT_DODO_CHEAT
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#define REGISTER_START_BUTTON
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#define REGISTER_START_BUTTON
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// Hud, frontend and radar
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// Hud, frontend and radar
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@ -1013,16 +1013,28 @@ CAutomobile::ProcessControl(void)
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m_aWheelSpeed[0] = Max(m_aWheelSpeed[0]-0.0005f, 0.0f);
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m_aWheelSpeed[0] = Max(m_aWheelSpeed[0]-0.0005f, 0.0f);
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}else if((GetModelIndex() == MI_DODO || CVehicle::bAllDodosCheat) &&
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}else if((GetModelIndex() == MI_DODO || CVehicle::bAllDodosCheat) &&
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m_vecMoveSpeed.Magnitude() > 0.0f && CTimer::GetTimeStep() > 0.0f){
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m_vecMoveSpeed.Magnitude() > 0.0f && CTimer::GetTimeStep() > 0.0f){
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#ifdef ALT_DODO_CHEAT
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if (bAltDodoCheat)
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FlyingControl(FLIGHT_MODEL_SEAPLANE);
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else
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#endif
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FlyingControl(FLIGHT_MODEL_DODO);
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FlyingControl(FLIGHT_MODEL_DODO);
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}else if(GetModelIndex() == MI_MIAMI_RCBARON){
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}else if(GetModelIndex() == MI_MIAMI_RCBARON){
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FlyingControl(FLIGHT_MODEL_RCPLANE);
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FlyingControl(FLIGHT_MODEL_RCPLANE);
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}else if(GetModelIndex() == MI_MIAMI_RCRAIDER || GetModelIndex() == MI_MIAMI_SPARROW || bAllCarCheat){
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}else if(GetModelIndex() == MI_MIAMI_RCRAIDER || GetModelIndex() == MI_MIAMI_SPARROW || bAllCarCheat){
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if(CPad::GetPad(0)->GetCircleJustDown())
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#ifdef ALLCARSHELI_CHEAT
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m_aWheelSpeed[0] = Max(m_aWheelSpeed[0]-0.03f, 0.0f);
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if (bAllCarCheat)
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if(m_aWheelSpeed[0] < 0.22f)
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m_aWheelSpeed[0] += 0.0001f;
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if(m_aWheelSpeed[0] > 0.15f)
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FlyingControl(FLIGHT_MODEL_HELI);
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FlyingControl(FLIGHT_MODEL_HELI);
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else
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#endif
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{
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if (CPad::GetPad(0)->GetCircleJustDown())
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m_aWheelSpeed[0] = Max(m_aWheelSpeed[0] - 0.03f, 0.0f);
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if (m_aWheelSpeed[0] < 0.22f)
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m_aWheelSpeed[0] += 0.0001f;
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if (m_aWheelSpeed[0] > 0.15f)
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FlyingControl(FLIGHT_MODEL_HELI);
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}
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}
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}
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}
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}
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@ -24,6 +24,9 @@ bool CVehicle::bAllDodosCheat;
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bool CVehicle::bCheat3;
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bool CVehicle::bCheat3;
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bool CVehicle::bCheat4;
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bool CVehicle::bCheat4;
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bool CVehicle::bCheat5;
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bool CVehicle::bCheat5;
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#ifdef ALT_DODO_CHEAT
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bool CVehicle::bAltDodoCheat;
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#endif
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bool CVehicle::m_bDisableMouseSteering = true;
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bool CVehicle::m_bDisableMouseSteering = true;
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void *CVehicle::operator new(size_t sz) { return CPools::GetVehiclePool()->New(); }
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void *CVehicle::operator new(size_t sz) { return CPools::GetVehiclePool()->New(); }
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@ -214,6 +217,19 @@ const CVector vecSeaAeroResistance(0.995f, 0.995f, 0.85f);
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const float fSpeedResistanceY = 500.0f;
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const float fSpeedResistanceY = 500.0f;
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const float fSpeedResistanceZ = 500.0f;
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const float fSpeedResistanceZ = 500.0f;
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const CVector vecHeliMoveRes(0.995f, 0.995f, 0.99f);
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const CVector vecRCHeliMoveRes(0.99f, 0.99f, 0.99f);
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const float fThrustVar = 0.3f;
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const float fRotorFallOff = 0.75f;
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const float fStabiliseVar = 0.015f;
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const float fPitchBrake = 10.0f;
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const float fPitchVar = 0.006f;
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const float fRollVar = 0.006f;
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const float fYawVar = -0.001f;
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const CVector vecHeliResistance(0.81f, 0.85f, 0.99f);
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const CVector vecRCHeliResistance(0.92f, 0.92f, 0.998f);
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const float fSpinSpeedRes = 20.0f;
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void
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void
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CVehicle::FlyingControl(eFlightModel flightModel)
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CVehicle::FlyingControl(eFlightModel flightModel)
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{
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{
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@ -332,7 +348,7 @@ CVehicle::FlyingControl(eFlightModel flightModel)
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fPitchImpulse = fRCTailMult * fTail * Abs(fTail) + fRCPitchMult * fSteerUD * fForwSpeed;
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fPitchImpulse = fRCTailMult * fTail * Abs(fTail) + fRCPitchMult * fSteerUD * fForwSpeed;
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else
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else
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fPitchImpulse = fSeaTailMult * fTail * Abs(fTail) + fSeaPitchMult * fSteerUD * fForwSpeed;
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fPitchImpulse = fSeaTailMult * fTail * Abs(fTail) + fSeaPitchMult * fSteerUD * fForwSpeed;
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ApplyTurnForce(fPitchImpulse* m_fTurnMass* GetUp()* CTimer::GetTimeStep(), vecWidthForward);
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ApplyTurnForce(fPitchImpulse * m_fTurnMass * GetUp() * CTimer::GetTimeStep(), vecWidthForward);
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float fLift = -DotProduct(GetMoveSpeed(), GetUp()) / Max(0.01f, GetMoveSpeed().Magnitude());
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float fLift = -DotProduct(GetMoveSpeed(), GetUp()) / Max(0.01f, GetMoveSpeed().Magnitude());
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float fLiftImpluse;
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float fLiftImpluse;
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@ -365,7 +381,76 @@ CVehicle::FlyingControl(eFlightModel flightModel)
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break;
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break;
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}
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}
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case FLIGHT_MODEL_HELI:
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case FLIGHT_MODEL_HELI:
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assert(0 && "Heli flight model not implemented");
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{
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CVector vecMoveResistance;
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if (GetModelIndex() == MI_MIAMI_SPARROW)
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vecMoveResistance = vecHeliMoveRes;
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else
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vecMoveResistance = vecRCHeliMoveRes;
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float rmX = Pow(vecMoveResistance.x, CTimer::GetTimeStep());
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float rmY = Pow(vecMoveResistance.y, CTimer::GetTimeStep());
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float rmZ = Pow(vecMoveResistance.z, CTimer::GetTimeStep());
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m_vecMoveSpeed.x *= rmX;
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m_vecMoveSpeed.y *= rmY;
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m_vecMoveSpeed.z *= rmZ;
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if (m_status != STATUS_PLAYER && m_status != STATUS_PLAYER_REMOTE)
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return;
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float fThrust;
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if (bCheat5)
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fThrust = CPad::GetPad(0)->GetSteeringUpDown() * fThrustVar / 128.0f + 0.95f;
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else
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fThrust = fThrustVar * (CPad::GetPad(0)->GetAccelerate() - 2 * CPad::GetPad(0)->GetBrake()) / 255.0f + 0.95f;
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fThrust -= fRotorFallOff * DotProduct(m_vecMoveSpeed, GetUp());
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#ifdef GTA3_1_1_PATCH
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if (fThrust > 0.9f && GetPosition().z > 80.0f)
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fThrust = 0.9f;
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#endif
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ApplyMoveForce(GRAVITY * GetUp() * fThrust * m_fMass * CTimer::GetTimeStep());
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if (GetUp().z > 0.0f)
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ApplyTurnForce(-CVector(GetUp().x, GetUp().y, 0.0f) * fStabiliseVar * m_fTurnMass * CTimer::GetTimeStep(), GetUp());
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float fRoll, fPitch, fYaw;
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if (bCheat5) {
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fPitch = CPad::GetPad(0)->GetCarGunUpDown() / 128.0f;
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fRoll = -CPad::GetPad(0)->GetSteeringLeftRight() / 128.0f;
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fYaw = CPad::GetPad(0)->GetCarGunLeftRight() / 128.0f;
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}
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else {
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fPitch = CPad::GetPad(0)->GetSteeringUpDown() / 128.0f;
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fRoll = CPad::GetPad(0)->GetLookLeft();
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if (CPad::GetPad(0)->GetLookRight())
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fRoll = -1.0f;
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fYaw = CPad::GetPad(0)->GetSteeringLeftRight() / 128.0f;
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}
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if (CPad::GetPad(0)->GetHorn()) {
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fYaw = 0.0f;
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fPitch = clamp(10.0f * DotProduct(m_vecMoveSpeed, GetUp()), -200.0f, 1.3f);
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fRoll = clamp(10.0f * DotProduct(m_vecMoveSpeed, GetRight()), -200.0f, 1.3f);
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}
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debug("fPitch: %f\n", fPitch);
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ApplyTurnForce(fPitch * GetUp() * fPitchVar * m_fTurnMass * CTimer::GetTimeStep(), GetForward());
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ApplyTurnForce(fRoll * GetUp() * fRollVar * m_fTurnMass * CTimer::GetTimeStep(), GetRight());
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ApplyTurnForce(fYaw * GetForward() * fYawVar * m_fTurnMass * CTimer::GetTimeStep(), GetRight());
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CVector vecResistance;
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if (GetModelIndex() == MI_MIAMI_SPARROW)
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vecResistance = vecHeliResistance;
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else
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vecResistance = vecRCHeliResistance;
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float rX = Pow(vecResistance.x, CTimer::GetTimeStep());
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float rY = Pow(vecResistance.y, CTimer::GetTimeStep());
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float rZ = Pow(vecResistance.z, CTimer::GetTimeStep());
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CVector vecTurnSpeed = Multiply3x3(m_vecTurnSpeed, GetMatrix());
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float fResistanceMultiplier = Pow(1.0f / (fSpinSpeedRes * SQR(vecTurnSpeed.z) + 1.0f), CTimer::GetTimeStep());
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float fResistance = vecTurnSpeed.z * fResistanceMultiplier - vecTurnSpeed.z;
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vecTurnSpeed.x *= rX;
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vecTurnSpeed.y *= rY;
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vecTurnSpeed.z *= rZ;
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m_vecTurnSpeed = Multiply3x3(GetMatrix(), vecTurnSpeed);
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ApplyTurnForce(-GetRight() * fResistance * m_fTurnMass, GetForward() + Multiply3x3(GetMatrix(), m_vecCentreOfMass));
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break;
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}
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}
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}
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}
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}
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@ -280,6 +280,9 @@ public:
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static bool bCheat3;
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static bool bCheat3;
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static bool bCheat4;
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static bool bCheat4;
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static bool bCheat5;
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static bool bCheat5;
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#ifdef ALT_DODO_CHEAT
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static bool bAltDodoCheat;
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#endif
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static bool m_bDisableMouseSteering;
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static bool m_bDisableMouseSteering;
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};
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};
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