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) β Gravitational parameter
a ((N,) array of floats) β Semi-major axis
e ((N,) array of floats) β Eccentricity
inc ((N,) array of floats) β Inclination (degrees)
capom ((N,) array of floats) β Longitude of the ascending node (degrees)
omega ((N,) array of floats) β Argument of periapsis (degrees)
capm ((N,) array of floats) β Mean anomaly (degrees)
- Returns:
rh ((N,3) array of floats) β position vector
vh ((N,3) array of floats)