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Merge branch 'master' of https://github.com/GTAmodding/re3

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This commit is contained in:
eray orçunus 2020-10-08 01:26:34 +03:00
commit 0409907438
2 changed files with 13 additions and 13 deletions
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24
src/vehicles/Vehicle.cpp
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@ -290,18 +290,18 @@ CVehicle::FlyingControl(eFlightModel flightModel)
case FLIGHT_MODEL_SEAPLANE: case FLIGHT_MODEL_SEAPLANE:
{ {
// thrust // thrust
float fThrust = flightModel == FLIGHT_MODEL_RCPLANE ? fRCAeroThrust : fSeaThrust;
float fThrustFallOff = flightModel == FLIGHT_MODEL_RCPLANE ? fRCPropFallOff : fSeaPropFallOff;
float fForwSpeed = DotProduct(GetMoveSpeed(), GetForward()); float fForwSpeed = DotProduct(GetMoveSpeed(), GetForward());
CVector vecTail = GetColModel()->boundingBox.min.y * GetForward(); CVector vecTail = GetColModel()->boundingBox.min.y * GetForward();
float fThrust = (CPad::GetPad(0)->GetAccelerate() - CPad::GetPad(0)->GetBrake()) / 255.0f; float fPedalState = (CPad::GetPad(0)->GetAccelerate() - CPad::GetPad(0)->GetBrake()) / 255.0f;
if (fForwSpeed > 0.1f || (flightModel == FLIGHT_MODEL_RCPLANE && fForwSpeed > 0.02f)) if (fForwSpeed > 0.1f || (flightModel == FLIGHT_MODEL_RCPLANE && fForwSpeed > 0.02f))
fThrust += 1.0f; fPedalState += 1.0f;
else if (fForwSpeed > 0.0f && fThrust < 0.0f) else if (fForwSpeed > 0.0f && fPedalState < 0.0f)
fThrust = 0.0f; fPedalState = 0.0f;
float fThrustAccel; float fThrustAccel = (fPedalState - fThrustFallOff * fForwSpeed) * fThrust;
if (flightModel == FLIGHT_MODEL_RCPLANE)
fThrustAccel = (fThrust - fRCPropFallOff * fForwSpeed) * fRCAeroThrust;
else
fThrustAccel = (fThrust - fSeaPropFallOff * fForwSpeed) * fSeaThrust;
ApplyMoveForce(fThrustAccel * GetForward() * m_fMass * CTimer::GetTimeStep()); ApplyMoveForce(fThrustAccel * GetForward() * m_fMass * CTimer::GetTimeStep());
// left/right // left/right
@ -353,12 +353,12 @@ CVehicle::FlyingControl(eFlightModel flightModel)
fPitchAccel = fSeaTailMult * fTail * Abs(fTail) + fSeaPitchMult * fSteerUD * fForwSpeed; fPitchAccel = fSeaTailMult * fTail * Abs(fTail) + fSeaPitchMult * fSteerUD * fForwSpeed;
ApplyTurnForce(fPitchAccel * m_fTurnMass * GetUp() * CTimer::GetTimeStep(), vecTail); ApplyTurnForce(fPitchAccel * m_fTurnMass * GetUp() * CTimer::GetTimeStep(), vecTail);
float fLift = -DotProduct(GetMoveSpeed(), GetUp()) / Max(0.01f, GetMoveSpeed().Magnitude()); float fLift = DotProduct(GetMoveSpeed(), GetUp()) / Max(0.01f, GetMoveSpeed().Magnitude()); //accel*angle
float fLiftAccel; float fLiftAccel;
if (flightModel == FLIGHT_MODEL_RCPLANE) if (flightModel == FLIGHT_MODEL_RCPLANE)
fLiftAccel = (fRCAttackLiftMult * fLift + fRCFormLiftMult) * fForwSpeed * fForwSpeed; fLiftAccel = (fRCFormLiftMult - fRCAttackLiftMult * fLift) * SQR(fForwSpeed);
else else
fLiftAccel = (fSeaAttackLiftMult * fLift + fSeaFormLiftMult) * fForwSpeed * fForwSpeed; fLiftAccel = (fSeaFormLiftMult - fSeaAttackLiftMult * fLift) * SQR(fForwSpeed);
float fLiftImpulse = fLiftAccel * m_fMass * CTimer::GetTimeStep(); float fLiftImpulse = fLiftAccel * m_fMass * CTimer::GetTimeStep();
if (GRAVITY * CTimer::GetTimeStep() * m_fMass < fLiftImpulse) { if (GRAVITY * CTimer::GetTimeStep() * m_fMass < fLiftImpulse) {
if (flightModel == FLIGHT_MODEL_RCPLANE && GetPosition().z > 50.0f) if (flightModel == FLIGHT_MODEL_RCPLANE && GetPosition().z > 50.0f)

2
vendor/librw vendored

@ -1 +1 @@
Subproject commit 30b77b0b32b4113b5dce2b67813ce9b85d1e1e57 Subproject commit edc77742c512b85ad35544b2cfbe3f359dc75805