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Leo satellites : dynamic modelling, simulations and some nonlinear attitude control techniques
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Date
2006
Author
Karataş, Soner
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In this thesis nonlinear control method techniques are investigated to control the attitude of Low Earth Orbit satellites. Nonlinear control methods are compared with linear control methods. Simulations are done using Matlab and Simulink software and BILSAT-1 parameters are used in the simulations. Reaction wheels are used as the actuator.
Subject Keywords
Electronics.
URI
http://etd.lib.metu.edu.tr/upload/12607196/index.pdf
https://hdl.handle.net/11511/15896
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Graduate School of Natural and Applied Sciences, Thesis
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S. Karataş, “Leo satellites : dynamic modelling, simulations and some nonlinear attitude control techniques,” M.S. - Master of Science, Middle East Technical University, 2006.
