In seconds.
When set to true, enable the default autopilot.
When set to an object, enable an autopilot with custom PID controls. All configuration is optional.
Leave empty to disbale the autopilot (same as false).
To move the center of mass of the aircraft
Contact properties must be specified for part types that declares collisionPoints.
A global drag coefficient.
Affect the spinning of propellers.
Ratio to affect the time it takes for the engine to reach a certain RPM value.
Positions in degrees for each flap step.
Number of positions for the flaps.
Seconds per degrees.
In seconds
Total mass in Kg.
Maximum RPM of the engine.
Minimum RPM of the engine.
Initial speed when in the air, in knots.
Ratio of head (camera) motion due to acceleration.
Part defined for the aircraft can be associated to a 3D model a node in the model or simply have a functional role (airfoil, engine, etc.).
Applicable properties vary with part's type (frame, airfoil, engine, wheel).
Are thrust reversers available.
For legacy reasons.
"startup" and "shutdown" sound ids are hardcoded.
Compensate for landing gear height at initialization (when on ground)
Initial tilt angle (when on ground).
In seconds - to match the startup sound.
Tweak the rotation inertia.
The altitude in feet at which the engine does not produce any thrust (linear from sea level).
Generated using TypeDoc
For some reason, GeoFS requires the definition to be an array, even though there is only one object.