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

fYear

2006

fDate

25-28 June 2006

Firstpage

1020

Lastpage

1024

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;

fLanguage

English

Publisher

ieee

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

Type

conf

DOI

10.1109/ICMA.2006.257765

Filename

4026225