DocumentCode
2252924
Title
Output control of spacecraft in leader follower formation
Author
Grøtli, Esten Ingar ; Chaillet, Antoine ; Gravdahl, Jan Tommy
Author_Institution
Dept. of Eng., Norwegian Univ. of Sci. & Technol., Trondheim, Norway
fYear
2008
fDate
9-11 Dec. 2008
Firstpage
1030
Lastpage
1035
Abstract
In this paper we will consider the control of spacecraft in a leader-follower formation using position measurements only. To analyze the formation under non vanishing disturbances, new definitions of practical exponential stability are given together with sufficient conditions for systems to satisfy these properties.
Keywords
aircraft control; multi-robot systems; stability; leader follower formation; position measurement; practical exponential stability; spacecraft control; Control systems; Error correction; Force control; Programmable control; Space vehicles; Stability analysis; Steady-state; Sufficient conditions; Time varying systems; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2008. CDC 2008. 47th IEEE Conference on
Conference_Location
Cancun
ISSN
0191-2216
Print_ISBN
978-1-4244-3123-6
Electronic_ISBN
0191-2216
Type
conf
DOI
10.1109/CDC.2008.4739295
Filename
4739295
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