Title :
Physical Simulation Experiment for Flexible Satellite Control with Accelerometer
Author :
Ying, Liu Ying ; Jun, Zhou ; Zhao, Din Jian
Author_Institution :
Coll. of Aeronaut., Northwestern Polytech. Univ., Xi´´an
Abstract :
The dynamic model of a physical simulation experiment system for flexible satellites is given. The measurement model of the accelerometer placed at the end of the flexible panel is established and an adaptive filter is used for its data processing. Feedback control using vibration information obtained from the accelerometer signal is designed. The physical simulation experiment results show that the control scheme is effective in vibration suppression
Keywords :
accelerometers; adaptive signal processing; artificial satellites; attitude control; control system synthesis; feedback; flexible structures; vibration control; accelerometer measurement model; adaptive filter; dynamic models; feedback control design; flexible panel; flexible satellite control; physical simulation experiment; vibration suppression; Accelerometers; Actuators; Adaptive filters; Control systems; Feedback control; Intelligent sensors; Satellites; Sensor systems; Signal design; Vibration control; accelerometer signal; flexible satellite; physical simulation experiment; vibration suppression;
Conference_Titel :
Mechatronics and Automation, Proceedings of the 2006 IEEE International Conference on
Conference_Location :
Luoyang, Henan
Print_ISBN :
1-4244-0465-7
Electronic_ISBN :
1-4244-0466-5
DOI :
10.1109/ICMA.2006.257765
