Challenges in the Stabilization of a Satellite Using Controlled Lagrangians I: Gravitation

被引：2
|
作者：
Haghi, Poorya [1 ]
Ghaffari-Saadat, Mohammad-Hassan [1 ]
机构：
[1] Amirkabir Univ Technol, Dept Mech Engn, Tehran, Iran
来源：
2009 IEEE CONTROL APPLICATIONS CCA & INTELLIGENT CONTROL (ISIC), VOLS 1-3 | 2009年
关键词：
MECHANICAL SYSTEMS; DYNAMICS;
D O I：
10.1109/CCA.2009.5281033
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 intends to study the stabilization of a satellite using the method of Controlled Lagrangians. The stability analysis of Euler-Poincare mechanical systems is extended to systems with non-zero potential energies. The results are then utilized in the stabilization of a satellite in a gravitational field. The effectiveness of the stabilizing law has been verified through simulations. In a sequel to this paper (Part II), we will extend the solution to an unbalanced satellite, and will discuss the capability of the method of Controlled Lagrangians to cope with the issue of actuator saturation.
引用
收藏
页码：764 / 769
页数：6
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