DocumentCode :
2034637
Title :
Orbital maintenance for observation mission of peanut-shaped asteroid
Author :
Bando, Mai ; Osuka, Koichi ; Fujii, Takao ; Yamakawa, Hiroshi
Author_Institution :
Unit of Synergetic Studies for Space, Kyoto Univ., Kyoto, Japan
fYear :
2011
fDate :
13-18 Sept. 2011
Firstpage :
1813
Lastpage :
1816
Abstract :
In this paper, we consider the motion control of spacecraft in the vicinity of the peanut-shaped asteroid. The implicit control concept is studied and orbital maintenance strategy to observe the peanut-shaped asteroid where the model of the gravity field is difficult to obtain is proposed. The implicit control law is characterized in terms of inverse problem of optimal control.
Keywords :
aerospace control; asteroids; celestial mechanics; motion control; optimal control; space vehicles; gravity field model; implicit control law; observation mission; optimal control inverse problem; orbital maintenance strategy; peanut-shaped asteroid; spacecraft motion control; Approximation methods; Conferences; Eigenvalues and eigenfunctions; Equations; Solar system; Space vehicles; Three dimensional displays; Selected keywords relevant to the subject;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
SICE Annual Conference (SICE), 2011 Proceedings of
Conference_Location :
Tokyo
ISSN :
pending
Print_ISBN :
978-1-4577-0714-8
Type :
conf
Filename :
6060260
Link To Document :
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