Guidance in the main deceleration section during a lunar landing of a spacecraft with an integrated propulsion system

DOI10.1134/S1064230716010111zbMath1383.93059MaRDI QIDQ1743042

V. P. Fedotov, D. A. Tuchin, A. G. Tuchin, V. N. Likhachev, Yu. G. Sikharulidze, B. I. Zhukov

Publication date: 12 April 2018

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

zbMATH Keywords

spacecraftlunar landing trajectoryintegrated propulsion systemmain deceleration sectionterminal guidance

Mathematics Subject Classification ID

Application models in control theory (93C95) Adaptive control/observation systems (93C40) Variable mass, rockets (70P05)

Related Items (1)

Guidance in the main deceleration section during a lunar landing of a spacecraft with an integrated propulsion system

Cites Work

• Guidance in the main deceleration section during a lunar landing of a spacecraft with an integrated propulsion system

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