Special control regime in the problem of optimal turn of an axially symmetric spacecraft-Reference-Cited by-同舟云学术

Special control regime in the problem of optimal turn of an axially symmetric spacecraft

Published:2010-12 Issue:6 Volume:49 Page:891-899
ISSN:1064-2307
Container-title:Journal of Computer and Systems Sciences International
language:en
Short-container-title:J. Comput. Syst. Sci. Int.

Author:

Molodenkov A. V.,Sapunkov Ya. G.

Publisher

Pleiades Publishing Ltd

Subject

Applied Mathematics,Computer Networks and Communications,Computer Vision and Pattern Recognition,Information Systems,Theoretical Computer Science,Control and Systems Engineering,Software

Link

http://link.springer.com/content/pdf/10.1134/S1064230710060079.pdf

Reference14 articles.

1. V. N. Branets and I. P. Shmyglevskii, Application of Quaternions in Problems of Orientation of Solid Bodies (Nauka, Moscow, 1973) [in Russian].

2. S. L. Scrivene and R. C. Thompson “Survey of Time-Optimal Attitude Maneuvers”, J. Guidance, Control, Dynamics. 17(2) (1994).

3. B. N. Petrov, V. A. Bodner, and K. B. Alekseev, “Analytical Solution of Control Problem of Spatial Rotation Maneuver” Dokl. Akad. Nauk SSSR, 192(6) (1970).

4. V. N. Branets, M. B. Chertok, and Yu. V. Kaznacheev, “Optimal Turn of a Solid Body with One Axis of Symmetry”, Kosmich. Issled., 22(3) (1984).

5. A. N. Sirotin, “Optimal Control of Re-Orientation of Symmetric Solid Body from Rest Position to Rest Position”, Izv. Ross. Akad. Nauk, Mekh. Tv. Tel., No. 1 (1989).

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