DocumentCode :
3446530
Title :
High-precision attitude control and active vibration suppression of flexible satellite
Author :
Zhi, Wang ; Ru-Fei, Zhang
Author_Institution :
Comput. Sci. & Eng. Coll., Xi´´an Technol. Univ., Xi´´an, China
Volume :
2
fYear :
2010
fDate :
29-31 Oct. 2010
Firstpage :
756
Lastpage :
761
Abstract :
A hybrid control scheme is proposed which combines the intelligent sliding mode control and vibration control. Considering the movement of flexible and rotating parts imposes large disturbances on the satellite, and affects the pointing accuracy and stability of attitude, a sliding mode controller is used to eliminate attitude error and ensure system stability. Self-recurrent wavelet neural network (SRWNN) is used to estimate sliding mode switching gain on-line, which can effectively weaken chattering caused by discontinuous sliding mode control. For actively damping the excited elastic vibrations, the strain-rate feedback control is also employed by using piezoelectric materials as additional sensors and actuators. Finally, simulation results indicate that the proposed hybrid controller provide a small steady error, a fast dynamic response, and an obvious rejection of flexible vibrations.
Keywords :
artificial satellites; attitude control; feedback; intelligent control; recurrent neural nets; strain control; variable structure systems; vibration control; flexible satellite; high precision attitude control; hybrid control; intelligent sliding mode control; piezoelectric material; self recurrent wavelet neural network; sliding mode controller; strain rate feedback control; vibration control; vibration suppression; Jacobian matrices; Robustness; SRWNN; active vibration suppression; flexible satellite; sliding mode control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Computing and Intelligent Systems (ICIS), 2010 IEEE International Conference on
Conference_Location :
Xiamen
Print_ISBN :
978-1-4244-6582-8
Type :
conf
DOI :
10.1109/ICICISYS.2010.5658643
Filename :
5658643
Link To Document :
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