Fixed-order dynamic compensation for a high-performance fighter aircraft

This paper presents a robust fixed-order dynamic compensator design for a high-performance fighter aircraft. The compensator design methodology is based on an approximate loop transfer recovery technique. Full-state gains are first designed for the dual system, which is the equivalent of designing a...

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Veröffentlicht in:Journal of guidance, control, and dynamics control, and dynamics, 1993-01, Vol.16 (1), p.104-110
Hauptverfasser: BYRNS, EDWARD V., CALISE, ANTHONY J.
Format: Artikel
Sprache:eng
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Zusammenfassung:This paper presents a robust fixed-order dynamic compensator design for a high-performance fighter aircraft. The compensator design methodology is based on an approximate loop transfer recovery technique. Full-state gains are first designed for the dual system, which is the equivalent of designing a full-order observer. Then the loop characteristics at the dual system input are approximated with a compensator in controller canonical form. Finally, the optimal gains are implemented in the dual compensator to insure robustness and tracking performance at the plant output. The fixed-order dynamic compensator developed here is compared with a previously published full-order observer design. (Author)
ISSN:0731-5090
1533-3884
DOI:10.2514/3.11433