Adaptive Flight Control Design with Optimal Control Modification for F-18 Aircraft Model-Reference-Cited by-同舟云学术

Adaptive Flight Control Design with Optimal Control Modification for F-18 Aircraft Model

Published:2010-04-20 Issue: Volume: Page:
ISSN:
Container-title:AIAA Infotech@Aerospace 2010
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Author:

Burken John¹,Nguyen Nhan²,Griffin Brian¹

Affiliation:

1. NASA Dryden Flight Research Center

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3364

Reference21 articles.

1. 1Burken,John,CurtisHanson,JamesLee,JohnKaneshige,“FlightTestComparisonofDifferentAdaptiveAugmentationsofFaultTolerant ControlLawsforaModifiedF-15Aircraft”,AIAAInfotech@AerospaceConference,AIAA-2009-2056.

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

3. Indirect adaptive flight control system interactions

4. 4Rysdyk,R.T.andCalise,A.J.“FaultTolerantFlightControlviaAdaptiveNeuralNetworkAugmentation”,AIAAGuidance,Navigation, andControlConference,AIAA-1998-4483,1998.

5. Nonlinear Flight Control Using Neural Networks

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