A comparison of neural, fuzzy, evolutionary, and adaptive approaches for carrier landing-Reference-Cited by-同舟云学术

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A comparison of neural, fuzzy, evolutionary, and adaptive approaches for carrier landing

Published:2001-08-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
language:
Short-container-title:

Author:

Page Anthony¹,Steinberg Marc¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-4085

Reference28 articles.

1. 2Egbert, L, Halley, I. "Stabilator Reconfiguration Flight Testing onthe F/A-18E/F,"2000.

2. Flight testing of a reconfigurable flight control law on the X-36 tailless fighter aircraft

3. 5Ward, D., Monaco, J., Barron, R., Bird, R., Virnig, J. "Self-Designing Controller: Design, Simulation, and Flight Test Evaluation,"USAF Report WL-TR-97-3095,Nov., 1996.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A L1 Adaptive Control Scheme for UAV Carrier Landing Using Nonlinear Dynamic Inversion;International Journal of Aerospace Engineering;2019-05-02

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