DocumentCode
3267362
Title
New method of capturing tumbling object in space and its control aspects
Author
Nakasuka, Shinichi ; Fujiwara, Takeshi
Author_Institution
Dept. of Aeronaut. & Astronaut., Tokyo Univ., Japan
Volume
2
fYear
1999
fDate
1999
Firstpage
973
Abstract
A method of capturing tumbling objects in a non-gravitational field is proposed, aiming at future on-orbit service missions such as capturing failed satellites or a manned vehicle which loses control, or removing debris. The key technology for this capture is how to compensate for the difference of rotational motions between the chaser and the target at the moment of capture. Most conventional methods use manipulator movement for this objective while keeping the position and attitude of the chaser body constant, which limits the allowable rotational velocity and patterns of the tumbling motion of the target. In the proposed method, the chaser aligns its rotational motion with the target´s one by appropriate control before capturing the target, which is expected to enlarge the allowable target rotational motion range. Technical issues to realize it are discussed and our approach to them are proposed, which is verified with some computer simulations and hardware experiments
Keywords
Lyapunov methods; aerospace control; aerospace simulation; artificial satellites; asymptotic stability; closed loop systems; conjugate gradient methods; feedback; motion control; optimal control; chaser; debris removal; failed satellites; manned vehicle; nongravitational field; on-orbit service missions; rotational motions; technical issues; tumbling object; Attitude control; Computer simulation; Hardware; Manipulators; Motion control; Orbital robotics; Satellites; Space missions; Space technology; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 1999. Proceedings of the 1999 IEEE International Conference on
Conference_Location
Kohala Coast, HI
Print_ISBN
0-7803-5446-X
Type
conf
DOI
10.1109/CCA.1999.800940
Filename
800940
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