Control Variables Parameterization Method of Powered Descent Trajectory for Lunar Explorer

被引:0
作者
Qiao, Yan-Di [1 ]
Zhang, Ze-Xu [1 ,2 ]
Deng, Han-Zhi [3 ]
Xu, Tian-Lai [1 ,2 ]
机构
[1] Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin,150001, China
[2] Shannxi Key Laboratory of Integrated and Intelligent Navigation, Xi'an,710000, China
[3] University of Jinan School of Electrical Engineering, Jinan,250022, China
来源
Yuhang Xuebao/Journal of Astronautics | 2021年 / 42卷 / 06期
关键词
Compilation and indexing terms; Copyright 2024 Elsevier Inc;
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学科分类号
摘要
Control vector parameterization - Descent trajectories - Dynamics modeling - Nonlinear programming methods - Optimal control problem - Parameterization method - Planning parameters - Three dimensional coordinate system
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页码:740 / 748
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