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This article is cited in 3 scientific papers (total in 3 papers)
Terminal control algorithm for descent from near-Earth orbit with landing in given region
Yu. G. Sikharulidze, A. N. Korchagin, A. S. Samotokhin, A. G. Tuchin
Abstract:
The reentry vehicle control for descent from near-Earth orbit under significant disturbances is considered. The method of automatically shift of de-orbit point as well as adaptation to real motion conditions and modification of reference roll function to satisfy given restrictions on landing accuracy, load factor and propellant consumption are suggested. The landing within restricted region of Russian Federation is provided.
Keywords:
terminal control, descent from near-Earth orbit, adaptation, load
factor and propellant reduce, landing within restricted region.
Citation:
Yu. G. Sikharulidze, A. N. Korchagin, A. S. Samotokhin, A. G. Tuchin, “Terminal control algorithm for descent from near-Earth orbit with landing in given region”, Keldysh Institute preprints, 2018, 046, 27 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2408 https://www.mathnet.ru/eng/ipmp/y2018/p46
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Abstract page: | 187 | Full-text PDF : | 203 | References: | 24 |
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