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Published Articles >> Table of Contents >> Abstract
First NASA/ESA Conference on Adaptive Hardware and Systems (AHS'06)
pp. 359-364
A Comparative Design of Satellite Attitude Control System with Reaction Wheel
Shengmin Ge, Harbin Institute of Technology, China
Hao Cheng, Harbin Institute of Technology, China
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DOI Bookmark: http://doi.ieeecomputersociety.org/10.1109/AHS.2006.2
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| Abstract |
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Reaction wheel is an important executive
component of satellite attitude control system. The
disturbance, which is caused by the reaction wheel
with a current controller, greatly influences the
accuracy and stability of satellite attitude control
system. To solve this problem, the idea of speed
feedback compensation control reaction wheel is put
forward. This paper introduces the design and
performance comparison of satellite attitude control
systems, which were separately based on current
control reaction wheel and speed feedback
compensation control reaction wheel. Analysis shows
that the speed feedback compensation control flywheel
system may effectively suppress torque fluctuation.
Simulation results indicate that the satellite attitude
control system with speed feedback compensation
control flywheel has improved performance.
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 Additional Information
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Citation:
Shengmin Ge, Hao Cheng,
"A Comparative Design of Satellite Attitude Control System with Reaction Wheel,"
ahs,
pp. 359-364,
First NASA/ESA Conference on Adaptive Hardware and Systems (AHS'06),
2006
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