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