Application of a Six Degree of Freedom Adaptive Controller to a General Aviation Aircraft-Reference-Cited by-同舟云学术

Application of a Six Degree of Freedom Adaptive Controller to a General Aviation Aircraft

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
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Author:

Lemon Kimberly¹,Steck James¹,Hinson Brian¹,Rokhsaz Kamran¹,Nguyen Nhan²

Affiliation:

1. Wichita State University

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6562

Reference10 articles.

1. Nonlinear Flight Control Using Neural Networks

2. 2Bosworth,J.,andWilliams-Hayes,P."FlightTestResultsfromtheNF-15BIntelligentFlightControlSystem(IFCs) Project with AdaptationtoaSimulated Stabilator Failure,"AIAA-2007-2818, AIAAInfotech@Aerospace, May2007.

3. 3Burken,J.,andKaneshige,J."ReconfigurableControlwithNeuralNetworkAugmentationforaModifiedF-15Aircraft," AIAA-2007-2823, AIAAInfotech@Aerospace, May2007.

4. 4Lemon,K.A.,Steck,J.E.,Hinson,B.T.,Nguyen,N.,Kimbal,D."ModelReferenceAdaptiveFightControlAdaptedfor General Aviation: Controller Gain Simulation andPreliminaryFlight Testingon aBonanzaFly-by-WireTestbed,"AIAA-2010-8278, AIAAGuidance, Navigation andControl, August2010.

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