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Entry Guidance with Terminal Time Control Based on Quasi-Equilibrium Glide Condition
IEEE Transactions on Aerospace and Electronic Systems ( IF 5.1 ) Pub Date : 2020-04-01 , DOI: 10.1109/taes.2019.2921213
Yuheng Guo , Xiang Li , Houjun Zhang , Linlin Wang , Ming Cai

The terminal constraints in entry guidance design are generally position and velocity constraints. In this study, the terminal time constraint is also taken into account. The estimates of time-to-go and range-to-go are discussed based on the quasi-equilibrium glide condition. Further analysis reveals that only two among the time-to-go, range-to-go, and terminal velocity are independent. Based on this observation, a guidance method is designed, which provides a new aspect to exploit the potential of entry guidance.

中文翻译:

基于准平衡下滑条件的终端时间控制进入引导

入口引导设计中的终端约束一般是位置和速度约束。在本研究中,还考虑了终端时间约束。基于准平衡滑翔条件讨论了飞行时间和飞行距离的估计。进一步的分析表明,飞行时间、飞行距离和终端速度中只有两个是独立的。基于这一观察,设计了一种引导方法,该方法为开发入门引导的潜力提供了一个新的方面。
更新日期:2020-04-01
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