Robust three-axis attitude stabilization for inertial pointing spacecraft using magnetorquers

被引：39
|
作者：
Celani, Fabio [1 ]
机构：
[1] Univ Roma La Sapienza, Dept Astronaut Elect & Energy Engn, I-00138 Rome, Italy
来源：
ACTA ASTRONAUTICA | 2015年 / 107卷
关键词：
Attitude control; Magnetic actuators; Averaging; Lyapunov stability; MAGNETIC ACTUATORS;
D O I：
10.1016/j.actaastro.2014.11.027
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In this work feedback control laws are designed for achieving three-axis attitude stabilization of inertial pointing spacecraft using only magnetic torquers. The designs are based on an almost periodic model of geomagnetic field along the spacecraft's orbit. Both attitude plus attitude rate feedback and attitude only feedback are proposed. Both feedback laws achieve local exponential stability robustly with respect to large uncertainties in the spacecraft's inertia matrix. The latter properties are proved using general averaging and Lyapunov stability. Simulations are included to validate the effectiveness of the proposed control algorithms. (C) 2014 IAA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码：87 / 96
页数：10
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