DocumentCode :
3006768
Title :
A quaternion-based adaptive attitude tracking controller without velocity measurements
Author :
Costic, B.T. ; Dawson, D.M. ; de Queiroz, M.S. ; Kapila, Vikram
Author_Institution :
Dept. of Electr. & Comput. Eng., Clemson Univ., SC, USA
Volume :
3
fYear :
2000
fDate :
2000
Firstpage :
2424
Abstract :
The main problem addressed in this paper is the quaternion-based, attitude tracking control of rigid spacecraft without angular velocity measurements and in the presence of an unknown inertia matrix. As a stepping-stone, we first design an adaptive, full-state feedback controller that compensates for parametric uncertainty while ensuring asymptotic attitude tracking errors. The adaptive, full-state feedback controller is then re-designed such that the need for angular velocity measurements is eliminated. The proposed adaptive, output feedback controller ensures asymptotic attitude tracking
Keywords :
adaptive control; asymptotic stability; attitude control; control system synthesis; space vehicles; state feedback; tracking; aerospace control; asymptotic stability; attitude control; inertia matrix; quaternion-based control; rigid spacecraft; state feedback; tracking; Adaptive control; Angular velocity; Angular velocity control; Attitude control; Error correction; Output feedback; Programmable control; Space vehicles; State feedback; Velocity measurement;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2000. Proceedings of the 39th IEEE Conference on
Conference_Location :
Sydney, NSW
ISSN :
0191-2216
Print_ISBN :
0-7803-6638-7
Type :
conf
DOI :
10.1109/CDC.2000.914164
Filename :
914164
Link To Document :
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