A comparison of intelligent, adaptive, and nonlinear flight control laws

Author:

Steinberg Marc1

Affiliation:

1. U.S. Navy, Naval Air Systems Command, Patuxent River, MD

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. (deg.) 1(deg.) Control Design Guidelines,"Final Report, WL-TR-96-3099, Aileron 145 1-25 I 100

2. Rudder 30 -30 82 Wright PattersonAFB, 1995. "Enns, D., Bugajski, R., Hendrick, R., Stein, G. "Dynamic Stabilator 10.5 -24 40 Inversion: An Evolving Methodology for Flight Control Table1- ActuatorRateandPositionLimits Design,"InternationalJournal of Control,January,1994. %rstic, M., Kanellakopoulos,I., Kokotovic, P.,Nonlinear and Size 1Roll )Alpha 1 AdaptiveControlDesign,JohnWiley & Sons,New York, 1995. 16-b.) 1(deg.) ?alise, A., Lee, S., Sharma, M."Direct Adaptive Small I5 IO Reconfigurable Control of a Tailless Fighter Aircrat?" Med. I60 IO I Proceedingsof the AIAA Guidance,Navigation, and Control Large 180 0 Conference,1998,pp. 88-97. Small 0 5 "Rysdyk, R., Calise, A. "Fault-Tolerant Flight Control via Small 0 -5 Adaptive Neural Network Augmentation,"Proceedingsof the Med. 0 15 AIAA Guidance,Navigation,and Control Conference,1998,pp. Med. 0 -15 1722-1728. 25Young,K., Utkin, V., Ozguner,U. "A Control Engineer's Large IO I30

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