* diminished by it affecting only 1/6th of the total, so it's an acceptable error.
*/
double thrustEstimate = store.thrustForce;
- store.thrustForce = calculateThrust(status, store.timestep, store.longitudalAcceleration,
+ store.thrustForce = calculateThrust(status, store.timestep, store.longitudinalAcceleration,
store.atmosphericConditions, true);
double thrustDiff = Math.abs(store.thrustForce - thrustEstimate);
// Log if difference over 1%, recompute if over 10%
double momZ = store.forces.getCroll() * dynP * refArea * refLength;
// Compute acceleration in rocket coordinates
- store.angularAcceleration = new Coordinate(momX / store.massData.getLongitudalInertia(),
- momY / store.massData.getLongitudalInertia(), momZ / store.massData.getRotationalInertia());
+ store.angularAcceleration = new Coordinate(momX / store.massData.getLongitudinalInertia(),
+ momY / store.massData.getLongitudinalInertia(), momZ / store.massData.getRotationalInertia());
store.rollAcceleration = store.angularAcceleration.z;
// TODO: LOW: This should be hypot, but does it matter?
}
if (store.massData != null) {
data.setValue(FlightDataType.TYPE_MASS, store.massData.getCG().weight);
+ data.setValue(FlightDataType.TYPE_LONGITUDINAL_INERTIA, store.massData.getLongitudinalInertia());
+ data.setValue(FlightDataType.TYPE_ROTATIONAL_INERTIA, store.massData.getRotationalInertia());
}
data.setValue(FlightDataType.TYPE_THRUST_FORCE, store.thrustForce);
public FlightConditions flightConditions;
- public double longitudalAcceleration = Double.NaN;
+ public double longitudinalAcceleration = Double.NaN;
public MassData massData;