ComputeInertialGravity

Declared in CelestialBody

Declaration

Vector3 ComputeInertialGravity(
    Vector3 inertialPosition,
    double step
);

Description

Calculates the gravity from this body at some location.

Parameters

Name	Description
inertialPosition	[m] The inertial reference frame location of the object.
step	[s] The time difference in step for spherical harmonics.