Magnetic torque attitude control of a satellite using the state-dependent Riccati equation technique

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Magnetic torque attitude control of a satellite using the state-dependent Riccati equation technique

A non-linear attitude control method for a satellite with magnetic torque rods using the state-dependent Riccati equation (SDRE) technique has been developed. The magnetic torque caused by the interaction with the Earth's magnetic field and the magnetic moment of torque rods plays a role of the...

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Bibliographic Details
Main Authors:	Mohammad Abdelrahman, Mohammad Ibraheem, Chang, Insu, Park, Sang-Young
Format:	Article
Language:	English
Published:	Elsevier 2011
Subjects:	TL787 Astronautics
Online Access:	http://irep.iium.edu.my/8581/ http://irep.iium.edu.my/8581/1/Abdelrahman_Magnetic_torque.pdf

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