DocumentCode :
286664
Title :
Flexible structure experiments at JPL and WPAFB: H controller designs
Author :
Smith, Malcolm C.
Author_Institution :
Dept. of Eng., Cambridge Univ., UK
fYear :
1993
fDate :
34134
Firstpage :
42401
Lastpage :
42406
Abstract :
A number of control system experiments were carried out during 1990 and 1991 on two contrasting flexible space structure facilities. The first facility is the JPL/AFAL flexible antenna in Pasadena, California. The second is the WPAFB/AFWL 12-meter cantilever truss in Dayton, Ohio. Each structure possesses a number of flexible modes of vibration which are lightly damped. The purpose of the experiments was to achieve active damping of the flexible modes via a digital control system. The control system designs were carried out using an H -based technique of `weighted gap optimization´, which is closely related to Glover-McFarlane loop-shaping
Keywords :
aerospace control; control system synthesis; damping; optimal control; vibration control; Glover-McFarlane loop-shaping; H controller; JPL/AFAL flexible antenna; WPAFB/AFWL; active damping; aerospace control; cantilever truss; control system designs; flexible space structure; optimal control; vibration control; weighted gap optimization;
fLanguage :
English
Publisher :
iet
Conference_Titel :
High Accuracy Platform Control in Space, IEE Colloquium on
Conference_Location :
London
Type :
conf
Filename :
255870
Link To Document :
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