Solutions of the second IEEE benchmark control problem [missile autopilot]

Author

Rimer, Melvyn ; Frederick, Dean K.

Author_Institution

Grumman Aircraft, Bethpage, NY, USA

fYear

1988

fDate

23-27 May 1988

Firstpage

401

Abstract

Results submitted for the continuous-time missile autopilot problem that was prepared by P. Hawley and T. Stevens (1986) are reported. The problem was released by the Benchmark Working Group of the IEEE Committee on Computer-Aided Control System Design (CACSD) to the control community at large in October 1987. The problem statement is described and the results submitted to date are summarized. This problem requires time simulations, pole and zero calculations, and frequency response plots for a linear, continuous-time system of relatively high order, specified as an interconnection of first- and second-order blocks. The problem comes in three levels of complexity, involving models having 13, 42, and 74 state variables. Plans for future benchmark problems are included

Keywords

aerospace computing; control system CAD; military computing; missiles; multivariable control systems; poles and zeros; program testing; IEEE benchmark control; continuous-time missile autopilot; control system CAD; frequency response plots; linear continuous system; multivariable control systems; pole and zero calculations; time simulations; Aircraft; Benchmark testing; Computer aided engineering; Continuous time systems; Control system synthesis; Control systems; Frequency response; Missiles; Packaging; Performance analysis;

fLanguage

English

Publisher

ieee

Conference_Titel

Aerospace and Electronics Conference, 1988. NAECON 1988., Proceedings of the IEEE 1988 National

Conference_Location

Dayton, OH

Type

conf

DOI

10.1109/NAECON.1988.195042

Filename

195042