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