DocumentCode
434585
Title
Robust attitude orbit control for large flimsy appendages
Author
Basso, Michele ; Rotunno, Max
Author_Institution
Dipartimento di Sistemi e Inf., Firenze Univ., Italy
Volume
1
fYear
2004
fDate
14-17 Dec. 2004
Firstpage
278
Abstract
The purpose of the paper is to present main results about design and simulation of an attitude orbit controller for a solar sail spacecraft with large flimsy appendages. The presence of a large number of uncertain flexible modes makes this problem suited for a robust control design based on quantitative feedback theory.
Keywords
attitude control; control system synthesis; feedback; robust control; space vehicles; large flimsy appendages; quantitative feedback theory; robust attitude orbit control; solar sail spacecraft; uncertain flexible modes; Attitude control; Control systems; Feedback; Payloads; Propulsion; Robust control; Space missions; Space technology; Space vehicles; Uncertain systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2004. CDC. 43rd IEEE Conference on
ISSN
0191-2216
Print_ISBN
0-7803-8682-5
Type
conf
DOI
10.1109/CDC.2004.1428643
Filename
1428643
Link To Document