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First NASA/ESA Conference on Adaptive Hardware and Systems (AHS'06)
A Comparative Design of Satellite Attitude Control System with Reaction Wheel
Istanbul, Turkey
June 15-June 18
ISBN: 0-7695-2614-4
ASCII Text
x 
 
Shengmin Ge, Hao Cheng, "A Comparative Design of Satellite Attitude Control System with Reaction Wheel," Adaptive Hardware and Systems, NASA/ESA Conference on, pp. 359-364, First NASA/ESA Conference on Adaptive Hardware and Systems (AHS'06), 2006.
 
 
BibTex
x
 
@article{ 10.1109/AHS.2006.2,
author = {Shengmin Ge and Hao Cheng},
title = {A Comparative Design of Satellite Attitude Control System with Reaction Wheel},
journal ={Adaptive Hardware and Systems, NASA/ESA Conference on},
volume = {0},
year = {2006},
isbn = {0-7695-2614-4},
pages = {359-364},
doi = {http://doi.ieeecomputersociety.org/10.1109/AHS.2006.2},
publisher = {IEEE Computer Society},
address = {Los Alamitos, CA, USA},
}
 
 
RefWorks Procite/RefMan/Endnote
x 
 
TY - CONF
JO - Adaptive Hardware and Systems, NASA/ESA Conference on
TI - A Comparative Design of Satellite Attitude Control System with Reaction Wheel
SN - 0-7695-2614-4
SP359
EP364
A1 - Shengmin Ge,
A1 - Hao Cheng,
PY - 2006
KW - null
VL - 0
JA - Adaptive Hardware and Systems, NASA/ESA Conference on
ER -
 
Shengmin Ge, Harbin Institute of Technology, China
Hao Cheng, Harbin Institute of Technology, China
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.
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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