Development of Adaptive Control Laws for Actuator Fault Accommodation-Reference-Cited by-同舟云学术

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Development of Adaptive Control Laws for Actuator Fault Accommodation

Published:2010-06-26 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
Short-container-title:

Author:

Tancredi Daniele¹,Gu Yu¹,Phillips Kerri¹,Gururajan Srikanth¹,Napolitano Marcello¹

Affiliation:

1. West Virginia University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-7547

Reference17 articles.

1. Hughes, David and Dornheim, Michael A. United DC-10 Crashes in Sioux City, Iowa. Aviation Week & Space Technology.July24,1989.

2. Burcham, Frank W., et al. Development and Flight Evaluation of an Emergency Digital Flight Control System UsingOnlyEngineThrustonan F-15Airplane.s.l.:NASA,1996.TechincalPaper3627.

3. Modeling and Model Reference Adaptive Control of Aircraft with Asymmetric Damage. Yiu, Liu and Tao, Gang, Joshi, SureshM. Chicago,IL :AIAA,Guidance,Navigation and ControlConference,2009.

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 discrete-time multivariable MRAC scheme applied to a nonlinear aircraft model with structural damage;Automatica;2015-03

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