Path: Orbit/OrbitManeuver
% Compute delta-Vs for rendezvous using Hohmann transfers.
The inputs are the target and chase spacecraft elements.
--------------------------------------------------------------------------
Form:
maneuver = HohmannTransferRendezvous( elT, elC, mu, tol, planet )
--------------------------------------------------------------------------
------
Inputs
------
elT (6,1) Target orbit elements
elC (6,1) Chase orbit elements
mu (1,1) Gravitational parameter
tol (1,1) Tolerance
planet (1,:) Planet name
-------
Outputs
-------
maneuver (1,1) Maneuver data structure
.dV1 (1,1) Transfer orbit insertion delta-V
.dV2 (1,1) Target orbit insertion delta-V
.tStart (1,1) Start time relative to epoch
.tTransfer (1,1) Time in transfer orbit
--------------------------------------------------------------------------