diff options
Diffstat (limited to 'src/vehicles/Vehicle.cpp')
| -rw-r--r-- | src/vehicles/Vehicle.cpp | 10 |
1 files changed, 5 insertions, 5 deletions
diff --git a/src/vehicles/Vehicle.cpp b/src/vehicles/Vehicle.cpp index 77c549f9..1132f79f 100644 --- a/src/vehicles/Vehicle.cpp +++ b/src/vehicles/Vehicle.cpp @@ -288,7 +288,7 @@ CVehicle::FlyingControl(eFlightModel flightModel) { // thrust float fForwSpeed = DotProduct(GetMoveSpeed(), GetForward()); - CVector vecWidthForward = GetColModel()->boundingBox.min.y * GetForward(); + CVector vecTail = GetColModel()->boundingBox.min.y * GetForward(); float fThrust = (CPad::GetPad(0)->GetAccelerate() - CPad::GetPad(0)->GetBrake()) / 255.0f; if (fForwSpeed > 0.1f || (flightModel == FLIGHT_MODEL_RCPLANE && fForwSpeed > 0.02f)) fThrust += 1.0f; @@ -311,13 +311,13 @@ CVehicle::FlyingControl(eFlightModel flightModel) fSideSlipAccel = Abs(fSideSpeed) * fSideSpeed * fSeaSideSlipMult; ApplyMoveForce(m_fMass * GetRight() * fSideSlipAccel * CTimer::GetTimeStep()); - float fYaw = -DotProduct(GetSpeed(vecWidthForward), GetRight()); + float fYaw = -DotProduct(GetSpeed(vecTail), GetRight()); float fYawAccel; if (flightModel == FLIGHT_MODEL_RCPLANE) fYawAccel = fRCRudderMult * fYaw * Abs(fYaw) + fRCYawMult * fSteerLR * fForwSpeed; else fYawAccel = fSeaRudderMult * fYaw * Abs(fYaw) + fSeaYawMult * fSteerLR * fForwSpeed; - ApplyTurnForce(fYawAccel * GetRight() * m_fTurnMass * CTimer::GetTimeStep(), vecWidthForward); + ApplyTurnForce(fYawAccel * GetRight() * m_fTurnMass * CTimer::GetTimeStep(), vecTail); float fRollAccel; if (flightModel == FLIGHT_MODEL_RCPLANE) { @@ -341,14 +341,14 @@ CVehicle::FlyingControl(eFlightModel flightModel) ApplyTurnForce(fStabiliseSpeed * m_fTurnMass * GetRight(), GetUp()); // no CTimer::GetTimeStep(), is it right? VC doesn't have it too // up/down - float fTail = -DotProduct(GetSpeed(vecWidthForward), GetUp()); + float fTail = -DotProduct(GetSpeed(vecTail), GetUp()); float fSteerUD = -CPad::GetPad(0)->GetSteeringUpDown() / 128.0f; float fPitchAccel; if (flightModel == FLIGHT_MODEL_RCPLANE) fPitchAccel = fRCTailMult * fTail * Abs(fTail) + fRCPitchMult * fSteerUD * fForwSpeed; else fPitchAccel = fSeaTailMult * fTail * Abs(fTail) + fSeaPitchMult * fSteerUD * fForwSpeed; - ApplyTurnForce(fPitchAccel * m_fTurnMass * GetUp() * CTimer::GetTimeStep(), vecWidthForward); + ApplyTurnForce(fPitchAccel * m_fTurnMass * GetUp() * CTimer::GetTimeStep(), vecTail); float fLift = -DotProduct(GetMoveSpeed(), GetUp()) / Max(0.01f, GetMoveSpeed().Magnitude()); float fLiftAccel; |