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Update(I)\n--------------------------------------------------------------------------------------------------\n\n--* Settings *--\n\nAimDownRange = 750 -- Range below missile will point directly at target\nPreDiveAltitude = 500 -- Altitude above target that missile will aim at before pointing at target\nSideAttackFactor = 0 -- Set how far missile will turn from target (0 is normal javelin style)\n\n--------------------------------------------------------------------------------------------------\n\n--* Advanced Settings *--\n\nAltitudeCorrectionFactor = 0 -- Higher vaules (Left missiles aim higher), Lower values (Right missiles aim higher)\n\n-------------------------------------------------------------------------------------------------\n\n  TargetPosition = I:GetTargetInfo(0, 0).AimPointPosition\n  TargetVelocity = I:GetTargetInfo(0, 0).Velocity\n\n  VehiclePosition = I:GetConstructCenterOfMass()\n  VehicleToTargetDistance = Vector3.Distance(TargetPosition, VehiclePosition)\n\n  SideAttackFactorOutputCorrection = SideAttackFactor * 1000/VehicleToTargetDistance \n  AltitudeCorrection = PreDiveAltitude * AltitudeCorrectionFactor * SideAttackFactor\n\n\n  for t=0, I:GetLuaTransceiverCount() - 1 do\n   for m=0, I:GetLuaControlledMissileCount(t) - 1 do\n\n      MissilePosition = I:GetLuaControlledMissileInfo(t, m).Position\n      MissileVelocity = Vector3.Magnitude(I:GetLuaControlledMissileInfo(t, m).Velocity)\n     \n      MissileToTargetDistance = Vector3.Distance(TargetPosition, MissilePosition)\n      TargetVector = Vector3.Normalize(TargetPosition - MissilePosition)\n\n\n    if t%2 == 1 then -- Right missiles\n     if MissileToTargetDistance > AimDownRange then\n\n     \n      ModifiedPointx = TargetPosition.z * SideAttackFactorOutputCorrection\n      ModifiedPointz = TargetPosition.x * SideAttackFactorOutputCorrection\n\n      TargetPositionNew = Vector3(ModifiedPointx,TargetPosition.y, ModifiedPointz)\n      TargetVectorNew = Vector3.Normalize(TargetPositionNew - MissilePosition)\n      MissileToTargetDistanceNew = Vector3.Distance(TargetPositionNew, MissilePosition)\n\n      RelativeVelocityMT = MissileVelocity - Vector3.Dot(TargetVectorNew, TargetVelocity)\n\n      MissilePrediction = TargetVelocity*MissileToTargetDistanceNew/RelativeVelocityMT\n      Point = TargetPosition + MissilePrediction - TargetPositionNew\n\n      MissileHitAltitude = TargetPosition.y + PreDiveAltitude - AltitudeCorrection\n\n      I:SetLuaControlledMissileAimPoint(t, m, Point.x, MissileHitAltitude, Point.z)\n\n     else\n       \n      RelativeVelocityMT = MissileVelocity - Vector3.Dot(TargetVector, TargetVelocity)\n\n      MissilePrediction = TargetVelocity*MissileToTargetDistance/RelativeVelocityMT\n      Point = TargetPosition + MissilePrediction\n\n      I:SetLuaControlledMissileAimPoint(t, m, Point.x, Point.y, Point.z)\n\n     end\n    end\n\n    if t%2 ==0 then -- Left missiles\n     if MissileToTargetDistance > AimDownRange then\n\n     \n      ModifiedPointx = TargetPosition.z * SideAttackFactorOutputCorrection\n      ModifiedPointz = TargetPosition.x * SideAttackFactorOutputCorrection\n\n      TargetPositionNew = Vector3(ModifiedPointx,TargetPosition.y, ModifiedPointz)\n      TargetVectorNew = Vector3.Normalize(TargetPositionNew - MissilePosition)\n      MissileToTargetDistanceNew = Vector3.Distance(TargetPositionNew, MissilePosition)\n\n      RelativeVelocityMT = MissileVelocity - Vector3.Dot(TargetVectorNew, TargetVelocity)\n\n      MissilePrediction = TargetVelocity*MissileToTargetDistanceNew/RelativeVelocityMT\n      Point = TargetPosition + MissilePrediction + TargetPositionNew\n\n      MissileHitAltitude = TargetPosition.y + PreDiveAltitude + AltitudeCorrection\n\n      I:SetLuaControlledMissileAimPoint(t, m, Point.x, MissileHitAltitude, Point.z)\n\n     else\n       \n      RelativeVelocityMT = MissileVelocity - Vector3.Dot(TargetVector, TargetVelocity)\n\n      MissilePrediction = TargetVelocity*MissileToTargetDistance/RelativeVelocityMT\n      Point = TargetPosition + MissilePrediction\n      \n      I:SetLuaControlledMissileAimPoint(t, m, Point.x, Point.y, Point.z)\n\n     end\n    end\n   end\n  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