Maintenance of the Halo Orbit for a Spacecraft Using Discrete-time Optimal Control —In the Framework of the Elliptic Restricted Three-body Problem—
Keisoku Jidō Seigyō Gakkai ronbunshū ; 54 , 2 ; 247-252
01.01.2018
6 pages
Aufsatz (Zeitschrift)
Unbekannt
DDC: | 629.8 |
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Formation Flying Along Halo Orbit of Circular-Restricted Three-Body Problem
Online Contents | 2015
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