A small-gain method for integrated guidance and control in terminal phase of reentry

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• 作者：Han Yan ; ^{yhbice@gmail.com} ; Shuping Tan ; Yingzi He
• 关键词：Reusable launch vehicles ; Approach and landing phase ; Reference trajectory ; Integrated guidance and control ; Small-gain theorem ; Robustness
• 刊名：Acta Astronautica
• 出版年：2017
• 出版时间：March 2017
• 年：2017
• 卷：132
• 期：Complete
• 页码：282-292
• 全文大小：1478 K
• 卷排序：132

文摘

A robust IGC law is designed for approach and landing of a RLV. The small-gain theorem is used to guarantee the stability of the overall system. It is proved that the closed-loop system has ISS property. The Monte Carlo simulation confirms the effectiveness of the proposed law.