|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
Path: Orbit/OrbitManeuver
% Compute the maneuver envelope for a spacecraft rotating around another. -------------------------------------------------------------------------- Form: [p, r] = ManeuverEnvelope( f, m ) -------------------------------------------------------------------------- ------ Inputs ------ f (:,1) Available force m (1,1) Mass ------- Outputs ------- p (1,:) Period r (1,:) Corresponding radius --------------------------------------------------------------------------
Common: Graphics/Plot2D
Back to the Orbit Module page