LUNAR_EXPLORATION

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Fuel-Optimal Trajectory Planning for Lunar Vertical Landing
《Guidance, Navigation and Control》2024年第2期123-140,共18页Kun Wang Zheng Chen Jun Li 
supported by the National Natural Science Foundation of China under grant Nos.61903331 and 62088101.
In this paper we consider a trajectory planning problem arising from a lunar vertical landing with minimum fuel consumption.The vertical landing requirement is written as a final steering angle constraint,and a nonneg...
关键词:Lunar exploration vertical soft landing final control constraint trajectory optimization indirect shooting method 
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