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Linearization in satellite attitude control with modified Rodriguez parameters
Date
2009-01-01
Author
Doruk, R. Özgür
Metadata
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Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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Purpose - The purpose of this paper is to analyze the results of the Jacobian matrix linearization of the satellite attitude dynamics with modified Rodriguez parameters (MRP) as attitude representation.
Subject Keywords
Kinematics
,
Control technology
,
Space technology
,
Artificial satellites
URI
https://hdl.handle.net/11511/64224
Journal
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
DOI
https://doi.org/10.1108/00022660910954691
Collections
Engineering, Article
Citation Formats
IEEE
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MLA
BibTeX
R. Ö. Doruk, “Linearization in satellite attitude control with modified Rodriguez parameters,”
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
, vol. 81, no. 3, pp. 199–203, 2009, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/64224.