DocumentCode :
1347081
Title :
Solutions of the second benchmark control problem
Author :
Rimer, Melvyn ; Frederick, Dean K. ; Huang, Chien Y.
Author_Institution :
Grumman Corp., Bethpage, NY, USA
Volume :
10
Issue :
5
fYear :
1990
Firstpage :
33
Lastpage :
39
Abstract :
A report is presented on the results of the second benchmark control problem prepared by the Benchmark Working Group of the IEEE Control Systems Society Technical Committee on computer-aided control system design (CACSD). The problem deals with a continuous-time missile autopilot design. The purpose of this benchmark is to provide a useful measure of some of the capabilities of computer-aided control system design packages. The problem requires time simulations, eigenvalue calculations, and frequency-response plots of relatively high-order linear systems. The problem is described, and the results submitted to date are summarized.<>
Keywords :
aerospace computing; aerospace control; control system CAD; eigenvalues and eigenfunctions; frequency response; missiles; Benchmark Working Group; aerospace control; autopilot design; benchmark control problem; control system CAD; eigenvalue; frequency-response plots; linear systems; missile; time simulations; Benchmark testing; Computational modeling; Control systems; Frequency; Laboratories; Missiles; Packaging; Physics; Societies; Software packages;
fLanguage :
English
Journal_Title :
Control Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0272-1708
Type :
jour
DOI :
10.1109/37.60422
Filename :
60422
Link To Document :
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