DocumentCode
2768790
Title
Output attitude control of flexible spacecraft from quaternion measures: a passivity approach
Author
Di Gennaro, S.
Author_Institution
Dipt. di Ingegneria Elettrica, l´´Aquila Univ., Italy
Volume
4
fYear
1998
fDate
16-18 Dec 1998
Firstpage
4549
Abstract
A dynamic controller is derived for a spacecraft with flexible appendages. The control aim is to design a control law that, using only attitude measures, allows for performing large angle manoeuvres. The approach is based on passivity concepts and the resulting controller ensures the asymptotic satisfaction of the control objectives and gives also estimates of the modal variables converging to the real values
Keywords
attitude control; control system synthesis; flexible structures; space vehicles; stability; dynamic controller; flexible appendages; flexible spacecraft; large angle manoeuvres; output attitude control; passivity approach; quaternion measures; Actuators; Angular velocity; Attitude control; Damping; Mathematical model; Performance evaluation; Quaternions; Space vehicles; Symmetric matrices; Wheels;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1998. Proceedings of the 37th IEEE Conference on
Conference_Location
Tampa, FL
ISSN
0191-2216
Print_ISBN
0-7803-4394-8
Type
conf
DOI
10.1109/CDC.1998.762042
Filename
762042
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