Minimum Fuel Guidance Law for the Powered Descending Phase of a Lunar Module

被引：0

作者：

Zhang, Feng ^{[1
]}

Duan, Guangren ^{[1
]}

Shan, Yongzheng ^{[1
]}

机构：

[1] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150006, Heilongjiang, Peoples R China

来源：

2009 IEEE INTERNATIONAL CONFERENCE ON AUTOMATION AND LOGISTICS ( ICAL 2009), VOLS 1-3 | 2009年

关键词：

Lunar Modules; Fuel Optimal Control; Parametric Guidance Law; Tracking Control; Parametric Eigenstructure Assignment Method;

D O I：

10.1109/ICAL.2009.5262953

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper deals with the fuel optimal control for the powered descending phase of a lunar module. Firstly, in the target coordinate frame, a 3-dimensional precise kinetic model is formulated. Secondly, the fuel optimal control problem for the powered descending phase is transformed into a standard constrained optimal control problem. By using a computational method and a time scaling transform technique, an open-loop parametric optimal guidance law is obtained. Then, to accurately track the minimum fuel orbit designed in the second step, based on parametric eigenstructure assignment method, a state feedback control law is derived. At last, the approach proves effective by numerical simulation.

引用

页码：152 / 157

页数：6

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