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authorNikolay Korolev <nickvnuk@gmail.com>2020-04-25 20:25:14 +0200
committerNikolay Korolev <nickvnuk@gmail.com>2020-04-25 20:25:14 +0200
commitae8deff1315f8535ebed4ae4a22d1dd7e808f3d0 (patch)
tree0b3bceea982c0b2d435322eda6922a34d83431ba /src/vehicles/Vehicle.cpp
parentMerge remote-tracking branch 'upstream/master' (diff)
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Diffstat (limited to 'src/vehicles/Vehicle.cpp')
-rw-r--r--src/vehicles/Vehicle.cpp89
1 files changed, 87 insertions, 2 deletions
diff --git a/src/vehicles/Vehicle.cpp b/src/vehicles/Vehicle.cpp
index a3bb705a..d0ccd31b 100644
--- a/src/vehicles/Vehicle.cpp
+++ b/src/vehicles/Vehicle.cpp
@@ -24,6 +24,9 @@ bool CVehicle::bAllDodosCheat;
bool CVehicle::bCheat3;
bool CVehicle::bCheat4;
bool CVehicle::bCheat5;
+#ifdef ALT_DODO_CHEAT
+bool CVehicle::bAltDodoCheat;
+#endif
bool CVehicle::m_bDisableMouseSteering = true;
void *CVehicle::operator new(size_t sz) { return CPools::GetVehiclePool()->New(); }
@@ -214,6 +217,19 @@ const CVector vecSeaAeroResistance(0.995f, 0.995f, 0.85f);
const float fSpeedResistanceY = 500.0f;
const float fSpeedResistanceZ = 500.0f;
+const CVector vecHeliMoveRes(0.995f, 0.995f, 0.99f);
+const CVector vecRCHeliMoveRes(0.99f, 0.99f, 0.99f);
+const float fThrustVar = 0.3f;
+const float fRotorFallOff = 0.75f;
+const float fStabiliseVar = 0.015f;
+const float fPitchBrake = 10.0f;
+const float fPitchVar = 0.006f;
+const float fRollVar = 0.006f;
+const float fYawVar = -0.001f;
+const CVector vecHeliResistance(0.81f, 0.85f, 0.99f);
+const CVector vecRCHeliResistance(0.92f, 0.92f, 0.998f);
+const float fSpinSpeedRes = 20.0f;
+
void
CVehicle::FlyingControl(eFlightModel flightModel)
{
@@ -332,7 +348,7 @@ CVehicle::FlyingControl(eFlightModel flightModel)
fPitchImpulse = fRCTailMult * fTail * Abs(fTail) + fRCPitchMult * fSteerUD * fForwSpeed;
else
fPitchImpulse = fSeaTailMult * fTail * Abs(fTail) + fSeaPitchMult * fSteerUD * fForwSpeed;
- ApplyTurnForce(fPitchImpulse* m_fTurnMass* GetUp()* CTimer::GetTimeStep(), vecWidthForward);
+ ApplyTurnForce(fPitchImpulse * m_fTurnMass * GetUp() * CTimer::GetTimeStep(), vecWidthForward);
float fLift = -DotProduct(GetMoveSpeed(), GetUp()) / Max(0.01f, GetMoveSpeed().Magnitude());
float fLiftImpluse;
@@ -365,7 +381,76 @@ CVehicle::FlyingControl(eFlightModel flightModel)
break;
}
case FLIGHT_MODEL_HELI:
- assert(0 && "Heli flight model not implemented");
+ {
+ CVector vecMoveResistance;
+ if (GetModelIndex() == MI_MIAMI_SPARROW)
+ vecMoveResistance = vecHeliMoveRes;
+ else
+ vecMoveResistance = vecRCHeliMoveRes;
+ float rmX = Pow(vecMoveResistance.x, CTimer::GetTimeStep());
+ float rmY = Pow(vecMoveResistance.y, CTimer::GetTimeStep());
+ float rmZ = Pow(vecMoveResistance.z, CTimer::GetTimeStep());
+ m_vecMoveSpeed.x *= rmX;
+ m_vecMoveSpeed.y *= rmY;
+ m_vecMoveSpeed.z *= rmZ;
+ if (m_status != STATUS_PLAYER && m_status != STATUS_PLAYER_REMOTE)
+ return;
+ float fThrust;
+ if (bCheat5)
+ fThrust = CPad::GetPad(0)->GetSteeringUpDown() * fThrustVar / 128.0f + 0.95f;
+ else
+ fThrust = fThrustVar * (CPad::GetPad(0)->GetAccelerate() - 2 * CPad::GetPad(0)->GetBrake()) / 255.0f + 0.95f;
+ fThrust -= fRotorFallOff * DotProduct(m_vecMoveSpeed, GetUp());
+#ifdef GTA3_1_1_PATCH
+ if (fThrust > 0.9f && GetPosition().z > 80.0f)
+ fThrust = 0.9f;
+#endif
+ ApplyMoveForce(GRAVITY * GetUp() * fThrust * m_fMass * CTimer::GetTimeStep());
+
+ if (GetUp().z > 0.0f)
+ ApplyTurnForce(-CVector(GetUp().x, GetUp().y, 0.0f) * fStabiliseVar * m_fTurnMass * CTimer::GetTimeStep(), GetUp());
+
+ float fRoll, fPitch, fYaw;
+ if (bCheat5) {
+ fPitch = CPad::GetPad(0)->GetCarGunUpDown() / 128.0f;
+ fRoll = -CPad::GetPad(0)->GetSteeringLeftRight() / 128.0f;
+ fYaw = CPad::GetPad(0)->GetCarGunLeftRight() / 128.0f;
+ }
+ else {
+ fPitch = CPad::GetPad(0)->GetSteeringUpDown() / 128.0f;
+ fRoll = CPad::GetPad(0)->GetLookLeft();
+ if (CPad::GetPad(0)->GetLookRight())
+ fRoll = -1.0f;
+ fYaw = CPad::GetPad(0)->GetSteeringLeftRight() / 128.0f;
+ }
+ if (CPad::GetPad(0)->GetHorn()) {
+ fYaw = 0.0f;
+ fPitch = clamp(10.0f * DotProduct(m_vecMoveSpeed, GetUp()), -200.0f, 1.3f);
+ fRoll = clamp(10.0f * DotProduct(m_vecMoveSpeed, GetRight()), -200.0f, 1.3f);
+ }
+ debug("fPitch: %f\n", fPitch);
+ ApplyTurnForce(fPitch * GetUp() * fPitchVar * m_fTurnMass * CTimer::GetTimeStep(), GetForward());
+ ApplyTurnForce(fRoll * GetUp() * fRollVar * m_fTurnMass * CTimer::GetTimeStep(), GetRight());
+ ApplyTurnForce(fYaw * GetForward() * fYawVar * m_fTurnMass * CTimer::GetTimeStep(), GetRight());
+
+ CVector vecResistance;
+ if (GetModelIndex() == MI_MIAMI_SPARROW)
+ vecResistance = vecHeliResistance;
+ else
+ vecResistance = vecRCHeliResistance;
+ float rX = Pow(vecResistance.x, CTimer::GetTimeStep());
+ float rY = Pow(vecResistance.y, CTimer::GetTimeStep());
+ float rZ = Pow(vecResistance.z, CTimer::GetTimeStep());
+ CVector vecTurnSpeed = Multiply3x3(m_vecTurnSpeed, GetMatrix());
+ float fResistanceMultiplier = Pow(1.0f / (fSpinSpeedRes * SQR(vecTurnSpeed.z) + 1.0f), CTimer::GetTimeStep());
+ float fResistance = vecTurnSpeed.z * fResistanceMultiplier - vecTurnSpeed.z;
+ vecTurnSpeed.x *= rX;
+ vecTurnSpeed.y *= rY;
+ vecTurnSpeed.z *= rZ;
+ m_vecTurnSpeed = Multiply3x3(GetMatrix(), vecTurnSpeed);
+ ApplyTurnForce(-GetRight() * fResistance * m_fTurnMass, GetForward() + Multiply3x3(GetMatrix(), m_vecCentreOfMass));
+ break;
+ }
}
}