AbsRelECI2Hills |
Compute a Hills state from a relative ECI state |
DeltaElem2Hills |
Computes the Hills frame state from orbital element differences and |
ECI2MeanElements |
Computes mean orbital elements from reference ECI position and velocity |
Goals2DeltaElem |
Computes the desired orbital element differences, given the formation flying |
Goals2Hills |
Compute a Hills state from geometric goals |
Hills2DeltaElem |
Computes the orbital element differences from the Hills frame state and the |
Osc2Mean |
Transforms osculating orbital elements to mean orbital elements. |