Declared in CelestialBody
Declaration
Vector3 ComputeInertialGravity(
Vector3 inertialPosition,
double step
);Description
Calculates the gravity from this body at some location.
Parameters
| Name | Description |
|---|---|
| inertialPosition | The inertial reference frame location of the object [m] |
| step | The time difference in step for spherical harmonics [s] |