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authoraap <aap@papnet.eu>2020-05-31 17:45:26 +0200
committeraap <aap@papnet.eu>2020-05-31 17:45:26 +0200
commitbae3a3e72f6b22b72155d377d38725cdbdff688c (patch)
tree09d9b2e732771ec71c9fe920a759930d50490eea /src/vehicles/Vehicle.cpp
parentfix (diff)
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Diffstat (limited to '')
-rw-r--r--src/vehicles/Vehicle.cpp10
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;