Satellite, Attitude Control by Quaternion-Based Backstepping

被引：184

作者：

Kristiansen, Raymond ^{[1
]}

Nicklasson, Per Johan ^{[1
]}

Gravdahl, Jan Tommy ^{[2
]}

机构：

[1] Narvik Univ Coll, Dept Comp Sci Elect Engn & Space Technol, N-8505 Narvik, Norway

[2] Norwegian Univ Sci & Technol, Dept Engn Cybernet, N-7491 Trondheim, Norway

来源：

IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY | 2009年 / 17卷 / 01期

关键词：

Attitude control; integrator backstepping; pulse width modulation; quaternion feedback; space vehicle control; FEEDBACK; STABILIZATION;

D O I：

10.1109/TCST.2008.924576

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

In this brief, a tracking controller is presented to stabilize the attitude of a micro satellite via integrator backstepping and quaternion feedback. The controller is shown to render the equilibrium points in the closed-loop system uniformly asymptotically stable. Simulations are performed using satellite parameters from the ESEO mission under the European Space Agency's SSETI project.

引用

页码：227 / 232

页数：6

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