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Vestnik SamGU. Estestvenno-Nauchnaya Ser., 2013, Issue 9/2(110), Pages 208–214
(Mi vsgu316)
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Mathematic Modeling
On the method of synthesis of optimal control of spacecraft reorientation during sensing hardware redirection
M. V. Morozova Institute for the Control of Complex Systems of RAS, Samara, 443020, Russian Federation
(published under the terms of the Creative Commons Attribution 4.0 International License)
Abstract:
The problem of optimal control of spacecraft reorientation during remote earth sensing hardware redirection is considered. Computational algorithm for the approximate solution of the problem is developed. Efficiency of this algorithm is confirmed by the results of the performed modeling.
Keywords:
spacecraft, remote Earth sensing, redirection, angular motion, optimal control, algorithms.
Received: 30.04.2013 Revised: 30.04.2013
Citation:
M. V. Morozova, “On the method of synthesis of optimal control of spacecraft reorientation during sensing hardware redirection”, Vestnik Samarskogo Gosudarstvennogo Universiteta. Estestvenno-Nauchnaya Seriya, 2013, no. 9/2(110), 208–214
Linking options:
https://www.mathnet.ru/eng/vsgu316 https://www.mathnet.ru/eng/vsgu/y2013/i92/p208
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Abstract page: | 174 | Full-text PDF : | 71 | References: | 41 |
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