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Downrange Estimation Based on Powered Explicit Guidance for Pinpoint Lunar Landing
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2021-11-25 , DOI: 10.1061/(asce)as.1943-5525.0001383 Haofan Wang 1 , Honghua Zhang 2 , Zeguo Wang 3 , Zhiwen Wang 3
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2021-11-25 , DOI: 10.1061/(asce)as.1943-5525.0001383 Haofan Wang 1 , Honghua Zhang 2 , Zeguo Wang 3 , Zhiwen Wang 3
Affiliation
Onboard computation of a fuel-optimal steering law is a pivotal technology for future
lunar and planetary campaigns with pinpoint landings. This paper proposes a method
of downrange estimation based on improved powered explicit guidance (PEG) ...
中文翻译：
基于动力显式制导的精确登月下距估计
燃料优化转向定律的机载计算是未来月球和行星运动精确着陆的关键技术。本文提出了一种基于改进动力显式引导 (PEG) ...
更新日期：2021-11-25
中文翻译：
基于动力显式制导的精确登月下距估计
燃料优化转向定律的机载计算是未来月球和行星运动精确着陆的关键技术。本文提出了一种基于改进动力显式引导 (PEG) ...
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