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

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• 作者：B. I. Zhukov ; V. N. Likhachev…
• 刊名：Journal of Computer and Systems Sciences International
• 出版年：2016
• 出版时间：March 2016
• 年：2016
• 卷：55
• 期：2
• 页码：260-270
• 全文大小：960 KB
• 刊物类别：Engineering
• 刊物主题：Control Engineering
  Russian Library of Science
  
• 出版者：MAIK Nauka/Interperiodica distributed exclusively by Springer Science+Business Media LLC.
• ISSN：1555-6530
• 卷排序：55

文摘

An algorithm is developed for terminal guidance during the main deceleration section of the lunar landing trajectory of a spacecraft with an integrated propulsion system, which has a main engine with variable thrust and four auxiliary nonthrottleable engines. A method of guidance adaptation to the actual motion conditions by measuring the thrust acceleration with jumps in time is proposed.Original Russian Text © B.I. Zhukov, V.N. Likhachev, Yu.G. Sikharulidze, A.G. Tuchin, D.A. Tuchin, V.P. Fedotov, 2016, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2016, No. 2, pp. 104–114.