Adaptive Gain-Scheduled Controllers in the Presence of Actuator Anomalies-Reference-Cited by-同舟云学术

Adaptive Gain-Scheduled Controllers in the Presence of Actuator Anomalies

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation and Control Conference and Exhibit
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Author:

Annaswamy Anuradha¹,Jang Jinho¹,Lavretsky Eugene²

Affiliation:

1. Massachusetts Institute of Technology

2. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7285

Reference16 articles.

1. 1KarlJ.AstromandBjornWittenmark. AdaptiveControl. Addison-Wesley,Reading,MA,2ndedition,1994.

2. 2Zachary T. Dydek, Himani Jain, Jinho Jang, and Anuradha M. Annaswamy. Theoretically verifiable stability margins for an adaptive controller. InProceedingsofAIAAGuidance,Navigation,andControlConference,Keystone,CO,2006.

3. 3DavidG.Wardetal. Flighttestresultsofanadaptiveguidancesystemforreusablelaunchvehicles. InProceedingsof2ndAIAAUnmanned UnlimitedSystemsSystems,Technologies,andOperations-Aerospace,Land,andSeaConferenceandWorkshop&Exhibit,2003.

4. 5Euclid. C. Holleman. Summary of high-altitude and entry flight control experience with the X-15 airplane. Technical Report TN D-3386, NASA,FlightResearchCenter,Edwards,California,April1966.

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