Control of angular motion of a landing module of “Soyuz” type upon satellite returning from the orbit-Reference-Cited by-同舟云学术

Control of angular motion of a landing module of “Soyuz” type upon satellite returning from the orbit

Published:2011-10 Issue:5 Volume:50 Page:826-836
ISSN:1064-2307
Container-title:Journal of Computer and Systems Sciences International
language:en
Short-container-title:J. Comput. Syst. Sci. Int.

Author:

Evdokimov S. N.,Klimanov S. I.,Komarova L. I.,Mikrin E. A.

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/S1064230711050078.pdf

Reference1 articles.

1. V. N. Branets, L. I. Komarova, E. A. Mikrin, et al., “A Control System for Landing “SoyuzTMA” Spacecraft,” Giroskop. Navigats., No. 3, 75–80 (2004).

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