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 |
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Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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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) |
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ISSN: | 0731-5090 1533-3884 |
DOI: | 10.2514/3.11433 |