DocumentCode
286660
Title
Simulated annealing applied to controlled design for large flexible space structures
Author
Rogers, E.
Author_Institution
Dept. of Aeronaut. & Astronautics, Southampton Univ., UK
fYear
1993
fDate
34134
Firstpage
42522
Lastpage
42523
Abstract
Summary form only given. Shows how simulated annealing can be applied to the controller placement problem for large scale linear time invariant systems under linear state feedback. Particular attention is paid to the four important-stages in the design of an algorithm based on this approach. Some initial results on the application of this approach to a large flexible space structure problems are presented together with some topics for short to medium term further research
Keywords
aerospace control; control system synthesis; feedback; large-scale systems; simulated annealing; aerospace control; controlled design; controller placement problem; large flexible space structures; linear state feedback; linear time invariant systems; simulated annealing;
fLanguage
English
Publisher
iet
Conference_Titel
High Accuracy Platform Control in Space, IEE Colloquium on
Conference_Location
London
Type
conf
Filename
255866
Link To Document