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Linearization in satellite attitude control with modified Rodriguez parameters

2009-01-01
Doruk, R. Özgür
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Creative Commons License
This work is licensed under a 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.
Kinematics, Control technology, Space technology, Artificial satellites
https://hdl.handle.net/11511/64224

Engineering, Article
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