Application of the Equinoctial Elements for Perturbation Approach to Orbit Raising (AAS 94-158)
Meeting, Spaceflight mechanics 1994 ; 1994 ; Cocoa Beach; FL
Spaceflight mechanics 1994 ; 367-378
ADVANCES IN THE ASTRONAUTICAL SCIENCES ; 87//pt1
1994-01-01
12 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Optimal low-thrust rendezvous using equinoctial orbit elements
Online Contents | 1996
|