swiftest.core.el2xv#
- swiftest.core.el2xv(mu, a, e, inc, capom, omega, capm)#
Convert orbital elements to state vectors
- Parameters:
mu ((N,) array of floats) – Gravitational parameter
a ((N,) array of floats) – Semi-major axis
e ((N,) array of floats) – Eccentricity
inc ((N,) array of floats) – Inclination (degrees)
capom ((N,) array of floats) – Longitude of the ascending node (degrees)
omega ((N,) array of floats) – Argument of periapsis (degrees)
capm ((N,) array of floats) – Mean anomaly (degrees)
- Returns:
rh ((N,3) array of floats) – position vector
vh ((N,3) array of floats)