Construction of the initial deorbit region for landing at the given place

DOI10.1134/S106423071702006XzbMath1385.93058MaRDI QIDQ1745815

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

Publication date: 18 April 2018

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

zbMATH Keywords

two-point boundary problemlandingdescent vehiclenominal deorbit point

Mathematics Subject Classification ID

Application models in control theory (93C95) Variable mass, rockets (70P05)

Cites Work

• Terminal control algorithm for the downrange motion of a descent module with load factor constraints
• Construction of the reachability region with regard to the attitude motion of a descent module at reentry with near-circular velocity
• Control of downrange and crossrange motion of a descent module in a certain range of reentry angles with load factor constraints

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