Optimal Two-Impulse Rendezvous Between Two Circular Orbits Using Multiple-Revolution Lambert's Solutions
AIAA Guidance, Navigation, and Control Conference and Exhibit
01.01.2002
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2002
|Optimal Two-Impulse Cotangent Rendezvous Between Coplanar Elliptical Orbits
Online Contents | 2013
|