Spacecraft relative rotation tracking without angular velocity measurements

被引：66

作者：

Kristiansen, Raymond ^{[1
]}

Loria, Antonio ^{[2
]}

Chaillet, Antoine ^{[3
]}

Nicklasson, Per Johan ^{[1
]}

机构：

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

[2] CNRS, LSS, F-91192 Gif Sur Yvette, France

[3] Univ Paris Sud Supelec EECI, F-91192 Gif Sur Yvette, France

来源：

AUTOMATICA | 2009年 / 45卷 / 03期

关键词：

Flight dynamics identification; Spacecraft formation; Quaternion feedback; Output-feedback control; Attitude control; OUTPUT-FEEDBACK CONTROL; BODY ATTITUDE TRACKING; CONTROLLERS;

D O I：

10.1016/j.automatica.2008.10.012

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

We present a solution to the problem of tracking relative rotation in a leader-follower spacecraft formation using feedback from relative attitude only. The controller incorporates an approximate-differentiation filter to account for the unmeasured angular velocity. We show uniform practical asymptotic stability (UPAS) of the closed-loop system. For simplicity, we assume that the leader is controlled and that we know orbital perturbations; however, this assumption can be easily relaxed to boundedness without degrading the stability property. We also assume that angular velocities of spacecraft relative to an inertial frame are bounded. Simulation results of a leader-follower spacecraft formation using the proposed controller structure are also presented. (C) 2008 Elsevier Ltd. All rights reserved.

引用

页码：750 / 756

页数：7

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