DocumentCode :
2983434
Title :
Design of tunable digital controllers incorporating dynamic pole-assignment compensators for high-performance aircraft
Author :
Porter, B. ; Boddy, C.L.
Author_Institution :
Dept. of Aeronaut. & Mech. Eng., Salford Univ., UK
fYear :
1988
fDate :
23-27 May 1988
Firstpage :
552
Abstract :
It is shown that tunable digital controllers can be readily enhanced so as to cope with one-loop unstable multivariable plants, which can be either nonminimum-phase or minimum-phase by incorporating dynamic pole-assignment compensators. Such inner-loop compensators facilitate the use of outer-loop PID controllers. The effectiveness of such a tunable digital controller is illustrated by designing a set-point tracking controller for the STOL/F-15 aircraft in a flight condition for which this aircraft is open-loop unstable
Keywords :
aerospace control; digital control; three-term control; STOL/F-15 aircraft; dynamic pole-assignment compensators; flight condition; high-performance aircraft; minimum-phase; nonminimum-phase; one-loop unstable multivariable plants; open-loop unstable; outer-loop PID controllers; set-point tracking controller; tunable digital controllers; Aerospace control; Aircraft; Asymptotic stability; Bismuth; Difference equations; Digital control; Open loop systems; Polynomials; Sampling methods; Three-term control;
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.1988.195061
Filename :
195061
Link To Document :
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