DocumentCode
1747449
Title
Robust attitude stabilization of spacecraft using minimal kinematic parameters
Author
Park, Yonmook ; Tahk, Min-Jea
Author_Institution
Dept. of Mech. Eng., Korea Advanced Inst. of Sci. & Technol., Taejeon, South Korea
Volume
2
fYear
2001
fDate
2001
Firstpage
1621
Abstract
We consider the problem of three-axis robust attitude stabilization of a rigid spacecraft using minimal, three-dimensional kinematic parameters. New nonlinear control laws having a class of related feedback gain structures are proposed, and are shown to provide a robustness with respect to inertia uncertainties of a rigid body. A numerical example is given to illustrate the theoretical results.
Keywords
asymptotic stability; attitude control; kinematics; robust control; space vehicles; feedback gain structures; inertia uncertainties; minimal kinematic parameters; nonlinear control laws; rigid spacecraft; robust attitude stabilization; robustness; Angular velocity; Attitude control; Feedback control; Kinematics; Orbital robotics; Quaternions; Robust control; Robustness; Space vehicles; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Robotics and Automation, 2001. Proceedings 2001 ICRA. IEEE International Conference on
ISSN
1050-4729
Print_ISBN
0-7803-6576-3
Type
conf
DOI
10.1109/ROBOT.2001.932843
Filename
932843
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