|
Vulcan
Aerospace Engineering Utilities Built on Janus
|
Classical Keplerian orbital elements. More...
#include <OrbitalTypes.hpp>
Public Attributes | |
| Scalar | a |
| Semi-major axis [m]. | |
| Scalar | e |
| Eccentricity [-]. | |
| Scalar | i |
| Inclination [rad]. | |
| Scalar | Omega |
| Right ascension of ascending node (RAAN) [rad]. | |
| Scalar | omega |
| Argument of periapsis [rad]. | |
| Scalar | nu |
| True anomaly [rad]. | |
Classical Keplerian orbital elements.
Standard six-element representation of an orbit in the two-body problem. All angles are in radians.
| Scalar vulcan::orbital::OrbitalElements< Scalar >::a |
Semi-major axis [m].
| Scalar vulcan::orbital::OrbitalElements< Scalar >::e |
Eccentricity [-].
| Scalar vulcan::orbital::OrbitalElements< Scalar >::i |
Inclination [rad].
| Scalar vulcan::orbital::OrbitalElements< Scalar >::nu |
True anomaly [rad].
| Scalar vulcan::orbital::OrbitalElements< Scalar >::Omega |
Right ascension of ascending node (RAAN) [rad].
| Scalar vulcan::orbital::OrbitalElements< Scalar >::omega |
Argument of periapsis [rad].