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Terminal control algorithm for the downrange motion of a descent module with load factor constraints

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Publication:395484
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DOI10.1134/S1064230712040041zbMath1282.93108MaRDI QIDQ395484

S. I. Klimanov, S. N. Evdokimov, A. N. Korchagin, Yu. G. Sikharulidze, E. A. Mikrin

Publication date: 29 January 2014

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)



Mathematics Subject Classification ID

Variable mass, rockets (70P05)


Related Items (6)

Unnamed Item ⋮ Control of downrange and crossrange motion of a descent module in a certain range of reentry angles with load factor constraints ⋮ Landing a descent module on the vostochnyi launch site after returning from the Moon ⋮ Construction of the initial deorbit region for landing at the given place ⋮ Construction of the reachability region with regard to the attitude motion of a descent module at reentry with near-circular velocity ⋮ A concept of the terminal descent control algorithm at reentry into the Earth atmosphere with near-parabolic velocity




Cites Work

  • Autonomous navigation system of near-Earth spacecraft




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