Spacecraft rendezvous trajectory between two elliptical orbits is determined by optimization of the two impulse orbital transfer
OPTIMUM TWO-IMPULSE ORBITAL TRANSFER AND RENDEZVOUS BETWEEN INCLINED ELLIPTICAL ORBITS
1963-08-21
Preprint
Keine Angabe
Englisch
Optimum low-thrust multiple rendezvous between inclined orbits
Elsevier | 1976
|Optimal Two-Impulse Cotangent Rendezvous Between Coplanar Elliptical Orbits
Online Contents | 2013
|