NDLI: Quaternion-based satellite attitude control

Content Provider	IEEE Xplore Digital Library
Author	Guang-Ren Duan
Copyright Year	2014
Description	Author affiliation: Center for Control Theor. & Guidance Technol., Harbin Inst. of Technol., Harbin, China (Guang-Ren Duan)
Abstract	In this paper, the dynamical model in a matrix second-order nonlinear form with respect to the quaternion coordinates is firstly established for the attitude system of a satellite, which is complete in the sense that no approximation is taken. Then, with the help of a recently proposed general parametric design approach for general fully-actuated second-order nonlinear systems, a direct parametric approach for satellite attitude control via proportional plus derivative quaternion feedback is proposed, which gives a complete parametrization of the pair of feedback gains. The approach possesses two important features. Firstly, with the proposed controller parametrization, the satellite attitude system, though highly nonlinear, can be turned into a constant linear system with desire eigenstructure. Secondly, in such a design there are still degrees of freedom which may be further utilized to improve the system performance. An example is considered to demonstrate the use of the proposed approach.
Starting Page	935
Ending Page	941
File Size	761546
Page Count	7
File Format	PDF
ISSN	20937121
e-ISBN	9788993215076
DOI	10.1109/ICCAS.2014.6987918
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2014-10-22
Publisher Place	South Korea
Access Restriction	Subscribed
Rights Holder	Institute of Control, Robotics and Systems (ICROS)
Subject Keyword	satellites nonlinear systems Satellites direct parametric approach Attitude control Field-flow fractionation quaternion representation Erbium
Content Type	Text
Resource Type	Article

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