DocumentCode
295182
Title
Symbolic algebraic discrete systems theory-applied to a fighter aircraft
Author
Plantin, Jonas ; Gunnarsson, Johan ; Germundsson, Roger
Author_Institution
Dept. of Electr. Eng., Linkoping Univ., Sweden
Volume
2
fYear
1995
fDate
13-15 Dec 1995
Firstpage
1863
Abstract
Symbolic algebraic modeling and analysis techniques for DEDS are applied to the landing gear subsystem in the new Swedish fighter aircraft, SAS 39 Gripen. The authors´ methods are based on polynomials over finite fields. Polynomials are used to represent the basic dynamic equations for the processes (controller and plant) as well as static properties of these. Temporal algebra (or temporal logic) is used to represent specifications of system behavior. The authors use this approach to model the landing gear controller from the complete implementation in Pascal. The authors also provide temporal algebra interpretations of the specifications made available to them. Finally the authors perform a number of symbolic analyses on the complete process (controller and plant). This project is a first demonstration of possible uses of these methods and tools and it shows that these methods and tools scale to a problem of a non-trivial size, i.e. of the size found in complex system designs such as the JAS 39
Keywords
aircraft control; discrete event systems; polynomials; temporal logic; DEDS; SAS 39 Gripen; fighter aircraft; landing gear subsystem; polynomials over finite fields; symbolic algebraic discrete systems theory; symbolic analyses; temporal algebra; temporal logic; Algebra; Equations; Galois fields; Gears; Logic functions; Military aircraft; Performance analysis; Polynomials; Process control; Synthetic aperture sonar;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
Conference_Location
New Orleans, LA
ISSN
0191-2216
Print_ISBN
0-7803-2685-7
Type
conf
DOI
10.1109/CDC.1995.480613
Filename
480613
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