Citation: | GUAN Ping, LIU Xiang-dong, CHEN Jia-bin. Adaptive Fuzzy Attitude Control of Flexible Satellite[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2005, 14(1): 50-54. |
[1] |
Wu S F, Eng elen C J H, Chu Q P. Fuzzy logic basedattitude control of the spacecraft X 38 along a nominal reentry trajector y[J]. Control Engineering Pract ice, 2001, 9(7):699-707.
|
[2] |
Steyn W H. F uzzy control for a non linear M IM O plantsubject to control constr ains[J]. IEEE T ransactions onSystem, M an, and Cybernet ics, 1994, 24(10):1565-1571.
|
[3] |
Qiao Xiro ng, Li Baoshou. A fuzzy neur al network controller and its application study for the spacecraft attitudecontrol system[J]. A er ospace Control, 1998, 16(1):13-18. (in Chinese)
|
[4] |
Chen Y ie chien, T eng Ching cheng. A model r eferencecontrol structure using a fuzzy neural network[J]. FuzzySets and System, 1995, 73:291-312.
|
[5] |
Zhang Renwei. Satellite orbital dynamics and attitudecontrol[M]. Beijing:Beijing U niversity of Aeronauticsand Astr onautics P ress, 1998. (in Chinese)
|
[6] |
T u Shancheng. Satellite attitude dynamics and control[M]. Beijing:Astronautic Publishing House, 1999. (inChinese)
|