Declared in Spacecraft
Declaration
void SetClassicElements(
double semiMajorAxis,
double eccentricity,
double inclination,
double omegaAscension,
double argumentOfPeriapsis,
double trueAnomaly,
string orbitingBody
);Description
Sets the classic elements of a body to a series of parameters based on the Keplerian elements.
Parameters
| Name | Description |
|---|---|
| semiMajorAxis | |
| eccentricity | |
| inclination | |
| omegaAscension | |
| argumentOfPeriapsis | |
| trueAnomaly | |
| orbitingBody | The name of the body orbiting |