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fixed flight control code
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bb14d9689f
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@ -202,7 +202,7 @@ const float fSeaPropFallOff = 2.3f;
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const float fSeaThrust = 0.002f;
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const float fSeaSideSlipMult = 0.1f;
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const float fSeaRudderMult = 0.01f;
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const float fSeaYawMult = 0.0003f;
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const float fSeaYawMult = -0.0003f;
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const float fSeaRollMult = 0.0015f;
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const float fSeaRollStabilise = -0.01f;
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const float fSeaPitchMult = 0.0002f;
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@ -316,7 +316,7 @@ CVehicle::FlyingControl(eFlightModel flightModel)
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CVector vecFRight = CrossProduct(GetForward(), CVector(0.0f, 0.0f, 1.0f));
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CVector vecStabilise = (GetUp().z > 0.0f) ? vecFRight : -vecFRight;
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float fStabiliseDirection = (GetUp().z > 0.0f) ? -1.0f : 1.0f;
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float fStabiliseDirection = (GetRight().z > 0.0f) ? -1.0f : 1.0f;
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float fStabiliseImpulse;
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if (flightModel == FLIGHT_MODEL_RCPLANE)
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fStabiliseImpulse = fRCRollStabilise * fStabiliseDirection * (1.0f - DotProduct(GetRight(), vecStabilise)) * (1.0f - Abs(GetForward().z));
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@ -332,14 +332,14 @@ CVehicle::FlyingControl(eFlightModel flightModel)
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fPitchImpulse = fRCTailMult * fTail * Abs(fTail) + fRCPitchMult * fSteerUD * fForwSpeed;
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else
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fPitchImpulse = fSeaTailMult * fTail * Abs(fTail) + fSeaPitchMult * fSteerUD * fForwSpeed;
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ApplyTurnForce(fPitchImpulse* m_fTurnMass* GetRight()* 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 fLiftImpluse;
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if (flightModel == FLIGHT_MODEL_RCPLANE)
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fLiftImpluse = (fRCAttackLiftMult * fLift + fRCFormLiftMult) * fForwSpeed * fForwSpeed;
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else
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fLiftImpluse = fSeaAttackLiftMult * fLift + fSeaFormLiftMult * fForwSpeed * fForwSpeed;
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fLiftImpluse = (fSeaAttackLiftMult * fLift + fSeaFormLiftMult) * fForwSpeed * fForwSpeed;
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float fLiftForce = fLiftImpluse * m_fMass * CTimer::GetTimeStep();
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if (GRAVITY * CTimer::GetTimeStep() * m_fMass < fLiftImpluse) {
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if (flightModel == FLIGHT_MODEL_RCPLANE && GetPosition().z > 50.0f)
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