DocumentCode :
2318701
Title :
Multivariable neural network vibration control based on output feedback
Author :
Boussalis, Dhemetrios ; Wang, Shyh Jong
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
1993
fDate :
13-16 Sep 1993
Firstpage :
345
Abstract :
This paper presents a multivariable direct adaptive control concept for vibration suppression in flexible space structures. The adaptive controller is implemented by a combination of forward neural networks. Tuning of the controller gains (neural network synaptic weights) takes place in real-time and is performed by a nonlinear least squares algorithm. The control scheme is based on output rather than state feedback, an approach motivated from the fact that, in most applications, the system state is not readily available. The results are demonstrated by simulation using a high fidelity 6-input 6-output dynamic model of the testbed at the JPL/USAF-PL Large Spacecraft Control Laboratory
Keywords :
aerospace control; distributed parameter systems; feedback; feedforward neural nets; large-scale systems; least squares approximations; multivariable control systems; vibration control; JPL/USAF-PL Large Spacecraft Control Laboratory; controller gain tuning; flexible space structures; forward neural networks; high fidelity 6-input 6-output dynamic model; multivariable direct adaptive control; multivariable neural network vibration control; neural network synaptic weights; nonlinear least squares algorithm; output feedback; vibration suppression; Adaptive control; Control systems; Least squares methods; Neural networks; Nonlinear dynamical systems; Performance gain; Programmable control; State feedback; Testing; Vibration control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications, 1993., Second IEEE Conference on
Conference_Location :
Vancouver, BC
Print_ISBN :
0-7803-1872-2
Type :
conf
DOI :
10.1109/CCA.1993.348267
Filename :
348267
Link To Document :
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