The Efficient Computation of Transfer Trajectories Between Earth Orbit and L~1 Halo Orbit Within the Framework of the Sun-Earth Restricted Circular Three Body Problem (AAS 00-174)
Annual space flight mechanics meeting ; 2000 ; Clearwater, MO
2000-01-01
22 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2000
|Formation Flying Along Halo Orbit of Circular-Restricted Three-Body Problem
Online Contents | 2015
|Sun-Earth L1 Region Halo-to-Halo Orbit and Halo-to-Lissajous Orbit Transfers
British Library Conference Proceedings | 2004
|