Six Degree of Freedom Variable Hierarchy Sliding Mode Control in Halo Orbits With Potential Function Guidance

被引：2
作者：
Lincoln, N. K. [1 ]
Veres, S. M. [1 ]
机构：
[1] Univ Southampton, Sch Engn Sci, Southampton SO9 5NH, Hants, England
来源：
47TH IEEE CONFERENCE ON DECISION AND CONTROL, 2008 (CDC 2008) | 2008年
关键词：
D O I：
10.1109/CDC.2008.4739404
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 presents a variable hierarchy six degree of freedom non-linear sliding mode controller for a satellite using potential function guidance for both position and attitude. The novelty is the formulation of the joint attitude/position sliding mode controller in combination with potential function guidance and proof of its asymptotic stability. The control method scales well to multiple satellite flying in formation with dynamic position and attitude requirements and as such is highly relevant to application is space systems such as interferometry. A target application of the acquisition and maintenance of a Halo type orbit about an unstable collinear Lagrange point, to a specified attitude, is obtained under the influence of the restricted three body dynamics.
引用
收藏
页码：1943 / 1949
页数：7
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