The problem of optimal control of the orientation of an orbit of a spacecraft as a deformable figure-Reference-Cited by-同舟云学术

The problem of optimal control of the orientation of an orbit of a spacecraft as a deformable figure

Published:2008-08 Issue:4 Volume:47 Page:621-634
ISSN:1064-2307
Container-title:Journal of Computer and Systems Sciences International
language:en
Short-container-title:J. Comput. Syst. Sci. Int.

Author:

Afanas’eva Yu. V.,Chelnokov Yu. N.

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/S106423070804014X.pdf

Reference7 articles.

1. Yu. N. Chelnokov, “Application of Quaternions in Problems of Optimal Control of the Motion of the Center of Mass of a Spacecraft in a Newtonian Gravitational Field. II,” Kosm. Issl. 41(1), 92–107 (2003).

2. Yu. N. Chelnokov, “Construction of Optimal Controls and Motion Trajectories of a Spacecraft that Uses a Quaternion Description of the Space Orientation of an Orbit,” Kosm. Issl. 35(5), 534–542 (1997).

3. V. A. Il’in and G. E. Kuzmak, Optimal Flights of Spacecraft (Nauka, Moscow, 1976) [in Russian].

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

5. Yu. N. Chelnokov, “Application of Quaternions in Problems of Optimal Control of the Motion of the Center of Mass of a Spacecraft in a Newtonian Gravitational Field. I,” Kosm. Issl. 39(5), 502–517 (2001).

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