double SpaceVehicle::getGrossWeight() const
{
double value = 0.0;
if (getDynamicsModel() != nullptr) {
value = getDynamicsModel()->getGrossWeight();
}
return value;
}
int SpaceVehicle::getEngThrust(double* const data, const int max) const
{
int n = 0;
if (getDynamicsModel() != nullptr) {
n = getDynamicsModel()->getEngThrust(data, max);
}
return n;
}
//------------------------------------------------------------------------------
// Get engine data: num engines, thrust, rpm, pla and fuel flow
//------------------------------------------------------------------------------
int SpaceVehicle::getNumberOfEngines() const
{
int n = 0;
if (getDynamicsModel() != nullptr) {
n = getDynamicsModel()->getNumberOfEngines();
}
return n;
}
//------------------------------------------------------------------------------
// atReleaseInit() -- Init weapon data at release
//------------------------------------------------------------------------------
void Missile::atReleaseInit()
{
// First the base class will setup the initial conditions
BaseClass::atReleaseInit();
if (getDynamicsModel() == 0) {
// set initial commands
cmdPitch = (LCreal) getPitch();
cmdHeading = (LCreal) getHeading();
cmdVelocity = vpMax;
if (getTargetTrack() != 0) {
// Set initial range and range dot
osg::Vec3 los = getTargetTrack()->getPosition();
trng = los.length();
trngT = trng;
}
else if (getTargetPlayer() != 0) {
// Set initial range and range dot
osg::Vec3 los = getTargetPosition();
trng = los.length();
trngT = trng;
}
else {
trng = 0;
}
// Range dot
trdot = 0;
trdotT = 0;
}
}
//------------------------------------------------------------------------------
// setTranslateYInput(transy) -- Translate Y inputs: normalized
// transy: -1.0 -> max left; 0.0 -> center; 1.0 -> max right
//------------------------------------------------------------------------------
bool SpaceVehicle::setTranslateYInput(const double transy)
{
bool ok = false;
SpaceDynamicsModel* model = dynamic_cast<SpaceDynamicsModel*>(getDynamicsModel());
if (model != nullptr) {
ok = model->setTranslateYInput(transy);
}
return ok;
}
//------------------------------------------------------------------------------
// setControlStickYawInput(yaw) -- Yaw inputs: normalized
// yaw: -1.0 -> max left; 0.0 -> center; 1.0 -> max right
//------------------------------------------------------------------------------
bool SpaceVehicle::setControlStickYawInput(const double yaw)
{
bool ok = false;
SpaceDynamicsModel* model = dynamic_cast<SpaceDynamicsModel*>(getDynamicsModel());
if (model != nullptr) {
ok = model->setControlStickYawInput(yaw);
}
return ok;
}
const AerodynamicsModel* AirVehicle::getAerodynamicsModel() const
{
return dynamic_cast<const AerodynamicsModel*>( getDynamicsModel() );
}
