DocumentCode
587383
Title
Attitude control of the spacecraft with unknown inertia tensor
Author
Surov, Maksim O. ; Pyrkin, Anton A. ; Bobtsov, Alexey A.
Author_Institution
Dept. of Control Syst. & Inf., St.-Petersburg Nat. Res. Univ. of Inf. Technol. Mech. & Opt., St. Petersburg, Russia
fYear
2012
fDate
3-5 Oct. 2012
Firstpage
820
Lastpage
824
Abstract
We propose the new robust control approach to solve the spacecraft attitude control problem. Obtained control low does not depend of inertia tensor components or its estimate. A proof of the asymptotic stability of the spacecraft orientation has been provided. To illustrate the effectiveness of the controller a numerical example is shown.
Keywords
asymptotic stability; attitude control; robust control; space vehicles; tensors; asymptotic stability; control law; inertia tensor components; robust control approach; spacecraft attitude control problem; spacecraft orientation; unknown inertia tensor; Adaptive control; Asymptotic stability; Attitude control; Quaternions; Space vehicles; Tensile stress; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications (CCA), 2012 IEEE International Conference on
Conference_Location
Dubrovnik
ISSN
1085-1992
Print_ISBN
978-1-4673-4503-3
Electronic_ISBN
1085-1992
Type
conf
DOI
10.1109/CCA.2012.6402414
Filename
6402414
Link To Document