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KIAM Preprint № 46, Moscow, 2018
Authors: Sikharulidze Y.G., Korchagin A. N., Samotokhin A. S., Tuchin A. G.
Terminal Control Algorithm for Descent from Near-Earth Orbit with Landing in Given Region
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
Publication language: russian,  pages: 27
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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About authors:
  • Sikharulidze Yury Georgievich,  KIAM RAS
  • Korchagin Andrey Nikolaevich,  orcid.org/0000-0002-9031-2723KIAM RAS
  • Samotokhin Alexander Sergeevich,  orcid.org/0000-0003-1523-7644KIAM RAS
  • Tuchin Andrey Georgievich,  orcid.org/0000-0002-9099-3100KIAM RAS