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Restore All Cars are Heli cheat

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This commit is contained in:
eray orçunus
2020-09-29 02:29:10 +03:00
parent a5d6c952a7
commit a0588ef8b1
7 changed files with 63 additions and 56 deletions
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51
src/vehicles/Vehicle.cpp
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@ -432,7 +432,12 @@ CVehicle::FlyingControl(eFlightModel flightModel)
case FLIGHT_MODEL_RCHELI:
case FLIGHT_MODEL_HELI:
{
float rm = Pow(pFlyingHandling->fMoveRes, CTimer::GetTimeStep());
#ifdef RESTORE_ALLCARSHELI_CHEAT
tFlyingHandlingData* flyingHandling = bAllCarCheat && GetStatus() == STATUS_PLAYER && !IsRealHeli() ? mod_HandlingManager.GetFlyingPointer(HANDLING_MAVERICK) : pFlyingHandling;
#else
tFlyingHandlingData* flyingHandling = pFlyingHandling;
#endif
float rm = Pow(flyingHandling->fMoveRes, CTimer::GetTimeStep());
m_vecMoveSpeed *= rm;
if (GetStatus() != STATUS_PLAYER && GetStatus() != STATUS_PLAYER_REMOTE)
return;
@ -441,11 +446,11 @@ CVehicle::FlyingControl(eFlightModel flightModel)
if(fThrust < 0.0f)
fThrust *= 2.0f;
if(flightModel == FLIGHT_MODEL_RCHELI){
fThrust = pFlyingHandling->fThrust * fThrust + 0.45f;
fThrust = flyingHandling->fThrust * fThrust + 0.45f;
ApplyMoveForce(GRAVITY * CVector(0.0f, 0.0f, 0.5f) * m_fMass * CTimer::GetTimeStep());
}else
fThrust = pFlyingHandling->fThrust * fThrust + 0.95f;
fThrust -= pFlyingHandling->fThrustFallOff * fUpSpeed;
fThrust = flyingHandling->fThrust * fThrust + 0.95f;
fThrust -= flyingHandling->fThrustFallOff * fUpSpeed;
if(flightModel == FLIGHT_MODEL_RCHELI && GetPosition().z > 40.0f)
fThrust *= 10.0f/(GetPosition().z - 30.0f);
else if(GetPosition().z > 80.0f)
@ -453,20 +458,20 @@ CVehicle::FlyingControl(eFlightModel flightModel)
ApplyMoveForce(GRAVITY * GetUp() * fThrust * m_fMass * CTimer::GetTimeStep());
if (GetUp().z > 0.0f){
float upRight = clamp(GetRight().z, -pFlyingHandling->fFormLift, pFlyingHandling->fFormLift);
float upImpulseRight = -upRight * pFlyingHandling->fAttackLift * m_fTurnMass * CTimer::GetTimeStep();
float upRight = clamp(GetRight().z, -flyingHandling->fFormLift, flyingHandling->fFormLift);
float upImpulseRight = -upRight * flyingHandling->fAttackLift * m_fTurnMass * CTimer::GetTimeStep();
ApplyTurnForce(upImpulseRight * GetUp(), GetRight());
float upFwd = clamp(GetForward().z, -pFlyingHandling->fFormLift, pFlyingHandling->fFormLift);
float upImpulseFwd = -upFwd * pFlyingHandling->fAttackLift * m_fTurnMass * CTimer::GetTimeStep();
float upFwd = clamp(GetForward().z, -flyingHandling->fFormLift, flyingHandling->fFormLift);
float upImpulseFwd = -upFwd * flyingHandling->fAttackLift * m_fTurnMass * CTimer::GetTimeStep();
ApplyTurnForce(upImpulseFwd * GetUp(), GetForward());
}else{
float upRight = GetRight().z < 0.0f ? -pFlyingHandling->fFormLift : pFlyingHandling->fFormLift;
float upImpulseRight = -upRight * pFlyingHandling->fAttackLift * m_fTurnMass * CTimer::GetTimeStep();
float upRight = GetRight().z < 0.0f ? -flyingHandling->fFormLift : flyingHandling->fFormLift;
float upImpulseRight = -upRight * flyingHandling->fAttackLift * m_fTurnMass * CTimer::GetTimeStep();
ApplyTurnForce(upImpulseRight * GetUp(), GetRight());
float upFwd = GetForward().z < 0.0f ? -pFlyingHandling->fFormLift : pFlyingHandling->fFormLift;
float upImpulseFwd = -upFwd * pFlyingHandling->fAttackLift * m_fTurnMass * CTimer::GetTimeStep();
float upFwd = GetForward().z < 0.0f ? -flyingHandling->fFormLift : flyingHandling->fFormLift;
float upImpulseFwd = -upFwd * flyingHandling->fAttackLift * m_fTurnMass * CTimer::GetTimeStep();
ApplyTurnForce(upImpulseFwd * GetUp(), GetForward());
}
@ -490,25 +495,25 @@ CVehicle::FlyingControl(eFlightModel flightModel)
fPitch = -CPad::GetPad(0)->GetCarGunUpDown() / 128.0f;
if (CPad::GetPad(0)->GetHorn()) {
fYaw = 0.0f;
fPitch = clamp(pFlyingHandling->fPitchStab * DotProduct(m_vecMoveSpeed, GetForward()), -200.0f, 1.3f);
fRoll = clamp(pFlyingHandling->fRollStab * DotProduct(m_vecMoveSpeed, GetRight()), -200.0f, 1.3f);
fPitch = clamp(flyingHandling->fPitchStab * DotProduct(m_vecMoveSpeed, GetForward()), -200.0f, 1.3f);
fRoll = clamp(flyingHandling->fRollStab * DotProduct(m_vecMoveSpeed, GetRight()), -200.0f, 1.3f);
}
ApplyTurnForce(fPitch * GetUp() * pFlyingHandling->fPitch * m_fTurnMass * CTimer::GetTimeStep(), GetForward());
ApplyTurnForce(fRoll * GetUp() * pFlyingHandling->fRoll * m_fTurnMass * CTimer::GetTimeStep(), GetRight());
ApplyTurnForce(fPitch * GetUp() * flyingHandling->fPitch * m_fTurnMass * CTimer::GetTimeStep(), GetForward());
ApplyTurnForce(fRoll * GetUp() * flyingHandling->fRoll * m_fTurnMass * CTimer::GetTimeStep(), GetRight());
float fSideSpeed = -DotProduct(GetMoveSpeed(), GetRight());
float fSideSlipAccel = pFlyingHandling->fSideSlip * fSideSpeed * Abs(fSideSpeed);
float fSideSlipAccel = flyingHandling->fSideSlip * fSideSpeed * Abs(fSideSpeed);
ApplyMoveForce(m_fMass * GetRight() * fSideSlipAccel * CTimer::GetTimeStep());
float fYawAccel = pFlyingHandling->fYawStab * fSideSpeed * Abs(fSideSpeed) + pFlyingHandling->fYaw * fYaw;
float fYawAccel = flyingHandling->fYawStab * fSideSpeed * Abs(fSideSpeed) + flyingHandling->fYaw * fYaw;
ApplyTurnForce(fYawAccel * GetRight() * m_fTurnMass * CTimer::GetTimeStep(), -GetForward());
ApplyTurnForce(fYaw * GetForward() * pFlyingHandling->fYaw * m_fTurnMass * CTimer::GetTimeStep(), GetRight());
ApplyTurnForce(fYaw * GetForward() * flyingHandling->fYaw * m_fTurnMass * CTimer::GetTimeStep(), GetRight());
float rX = Pow(pFlyingHandling->vecTurnRes.x, CTimer::GetTimeStep());
float rY = Pow(pFlyingHandling->vecTurnRes.y, CTimer::GetTimeStep());
float rZ = Pow(pFlyingHandling->vecTurnRes.z, CTimer::GetTimeStep());
float rX = Pow(flyingHandling->vecTurnRes.x, CTimer::GetTimeStep());
float rY = Pow(flyingHandling->vecTurnRes.y, CTimer::GetTimeStep());
float rZ = Pow(flyingHandling->vecTurnRes.z, CTimer::GetTimeStep());
CVector vecTurnSpeed = Multiply3x3(m_vecTurnSpeed, GetMatrix());
float fResistanceMultiplier = Pow(1.0f / (pFlyingHandling->vecSpeedRes.z * SQR(vecTurnSpeed.z) + 1.0f) * rZ, CTimer::GetTimeStep());
float fResistanceMultiplier = Pow(1.0f / (flyingHandling->vecSpeedRes.z * SQR(vecTurnSpeed.z) + 1.0f) * rZ, CTimer::GetTimeStep());
float fResistance = vecTurnSpeed.z * fResistanceMultiplier - vecTurnSpeed.z;
vecTurnSpeed.x *= rX;
vecTurnSpeed.y *= rY;