Robust lateral-directional control design for the F/A-18

1999 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1999, Pages 1213-1219

  Tu, K Y ^a   Sideris, A ^a   Mease, K D ^a   Nathan, J ^a   Carter, J ^b  

^a University of California at Irvine   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOMBERS; CONTROL THEORY; CONTROLLERS; DESIGN; LINEAR CONTROL SYSTEMS; ROBUST CONTROL; SUPERSONIC AIRCRAFT;

CONTROL LAW DESIGN; DIRECTIONAL CONTROL; DYNAMIC PRESSURES; LINEAR CONTROLLERS; PERFORMANCE MODEL; ROBUST CONTROL DESIGNS; ROBUST CONTROLLERS; SIMULATED RESPONSE;

FIGHTER AIRCRAFT;

EID: 84902135884     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Numerous authors from Honeywell and Lockheed Martin, “Application of Multivariable Control Theory to Aircraft Control Laws (Multivariable Control Design Guidelines),” WL-TR-96-3099, May 1996.
2. Reiner, J., Balas, G. J., and Garrard, W. L., “Flight Control Design Using Robust Dynamic Inversion and Time-Scale Separation,” Automatica, Vol. 32, No. 11, 1996, pp. 1493-1504.
3. Lee, L. H. and Spillman, M., “Robust, Reduced-Order, Linear Parameter-Varying Flight Control for an F-16,” Paper AIAA-97-3637, 1997.
4. Ngo, A. N., Reigelsperger, W. C. and Banda, S. S., “Multivariable Control Law Design for a Tailless Aircraft,” Paper AIAA 96-3866, 1996.
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9. Balas, G., Doyle, J., Glover, K., Packard, A. and Smith, R., “p-Tools. Matlab Functions for the Analysis and Design of Robust Control Systems,” Musyn Inc., P. O. Box 1337, Minneapolis, MN 55414-5377, 1991.
10. Balas, G., et al., “Control of the F-14 Aircraft Lateral-Directional Axis During Powered Approach,” J. Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 899-908.
11. Hodgkinson, J., Aircraft Handling Qualities, AIAA, Reston, 1999.