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
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;
Conference_Titel :
Control Applications (CCA), 2012 IEEE International Conference on
Conference_Location :
Dubrovnik
Print_ISBN :
978-1-4673-4503-3
Electronic_ISBN :
1085-1992
DOI :
10.1109/CCA.2012.6402414
