A Microsatellite Reaction Wheel Based on a Fuzzy Logic Controller for the Attitude Control System
Current interest in small satellites lies in the feasibility of achieving specific but limited objectives, by necessity, small satellites technology requires simple control schemes. In this paper, we present a fuzzy logic controller, as an attempt to replace the classical proportional derivative (PD) controller that is widely used in the spacecraft attitude determination control system (ADCS). The fuzzy logic controller is implemented on the Z axis (yaw) closed loop reaction wheel of a low earth orbit microsatellite with a gravity gradient stabilization. The yaw axis is pointed toward earth. We mention here that, when the spacecraft is not in the imaging mode, it starts spinning along the yaw axis to keep it within thermal limits. So that, in this axis the spacecraft is either in the imaging mode (freeze mode) or barbeque mode (BBQ mode).
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Passino , M. Kevin S.Yurkovich, “Fuzzy Control” Addison-Wesley 1998.
H.B. Verbruggen, P.M. Brujin, “Fuzzy Control and Conventional Control – What is the real contribution of Fuzzy Systems” Fuzzy Sets and Systems 1997 (151-160).
A. Visioli “Tuning of PID controllers with fuzzy logic” IEEE Proc.-Control Theory Appl., Vol.148, No.1, January 2001
S. A. Erbay “An overview of Fuzzy Logic” R.T.P. Corporation, Pompano Beach, Florida, U.S.A.
K. Suwat, S. Kuntanapreeda, “Model Reference fuzzy Control of Nonlinear System” International conference on Robotics, Vision and Parallel Processing for Industrial Automation, Ipoh,Perak,Malaysia,Nov.1996.
K. R. Berenji, R. N. Lea, Y. Jani, P. Khedkar, A. Malkani, J. Hobiit,”Space Shuttle Attitude Control by Reinforcernent Learning and Fuzzy Logic” 1993 IEEE International Conference on Fuzzy- Systems. Vol. 2, pp. 1396- 1401.
R. Y .Chiang, J.-S. R. Jang, “Fuzzy Logic Attitude Control for Cassini Spacecraft” 1994 IEEE International Conference on Fuzzy Systems, Vol. 3, pp. 1532-1537.
Y. Matsuzaki, S.Abe, “Fuzzy Logic Control of Three-Dimensional Motion of a Tethered Satellite System” Proceedings of the AIAA/ASMUAHS/ASC Strucrures, Structural Dynamics. and Material Conference, Vol. 4. 1994. New York.NY, USA. AIAA-94- I6 17-CP. pp. 2378-2383.
W. H. Steyn, “Comparison of Low-Earth-Orbit Satellite Controllers Submitted to Controllability Constraints” Journal of Guidance. Control and Dynamics, Vol. 17,NO. 4, pp. 795-804. 1994.
W. Pedryez, J.F. Peters, S. Ramanna, “Hierarchical Fuzzy Neural Attitude Control for Satellites”, IEEE,1997.
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