DocumentCode :
2129870
Title :
Vibration damping and robust control of the JPL/AFAL experiment using μ-synthesis
Author :
Balas, Gary J. ; Chu, Cheng-Chih ; Doyle, John C.
Author_Institution :
Aeronaut. Eng., California Inst. of Technol., Pasadena, CA, USA
fYear :
1989
fDate :
13-15 Dec 1989
Firstpage :
2689
Abstract :
The technology for controlling elastic deformations of flexible structures is one of the key considerations for future space initiatives. A vital area needed to achieve this objective is the development of a control design methodology applicable to future structures. The μ-synthesis technique is employed to design a high-performance vibration attenuation controller for the JPL/AFAL experimental flexible antenna structure. The results presented deal primarily with the control of first two global flexible modes using only two hub actuators and two hub sensors. Implementation of the multivariable control laws based on a finite-element model is presented. All results are from actual implementation on the JPL/AFAL flexible structure testbed
Keywords :
aerospace control; antennas; control system synthesis; multivariable control systems; vibration control; JPL/AFAL; aerospace control; control design; control system synthesis; elastic deformations; experimental flexible antenna structure; finite-element model; hub actuators; hub sensors; multivariable control; vibration damping; Actuators; Attenuation; Control design; Damping; Finite element methods; Flexible structures; Robust control; Space technology; Testing; Vibration control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1989., Proceedings of the 28th IEEE Conference on
Conference_Location :
Tampa, FL
Type :
conf
DOI :
10.1109/CDC.1989.70668
Filename :
70668
Link To Document :
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