Real-Time System Identification of a Small Multi-Engine Aircraft with Structural Damage-Reference-Cited by-同舟云学术

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Real-Time System Identification of a Small Multi-Engine Aircraft with Structural Damage

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

Chowdhary Girish¹,DeBusk Wesley¹,Johnson Eric¹

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3472

Reference9 articles.

1. Real-Time Dynamic Modeling: Data Information Requirements and Flight Test Results

2. AIAAEducation Series;Klein V.,2006

3. In-flight system identification

4. NelsonR.C."FlightStabilityandAutomaticControl,"McGrawHillHigherEducation,1998.

5. MULTIPLEXModellsportGmbHKG.MainCatalogue,TechnicalReport,2007.

Cited by 4 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. Inflight Parameter Estimation Framework for Fixed-Wing UAV;Lecture Notes in Mechanical Engineering;2018-12-15

2. Aerodynamic System Identification of Fixed-wing UAV;AIAA Atmospheric Flight Mechanics (AFM) Conference;2013-08-15

3. Guidance and Control of Airplanes Under Actuator Failures and Severe Structural Damage;Journal of Guidance, Control, and Dynamics;2013-07

4. Sequential Aerodynamic Model Parameter Identification;IFAC Proceedings Volumes;2012-07

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