Simulation and Adaptive Control of a High Agility Model Airplane in the Presence of Severe Structural Damage and Failures-Reference-Cited by-同舟云学术

Simulation and Adaptive Control of a High Agility Model Airplane in the Presence of Severe Structural Damage and Failures

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

Baur Stephan¹,Annaswamy Anuradha¹,Gibson Travis¹,Höcht Leonhard²,Holzapfel Florian²

Affiliation:

1. Massachusetts Institute of Technology

2. Technical University of Munich

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6412

Reference24 articles.

1. 1NarendraKS,AnnaswamyAM(1989)StableAdaptiveSystems.DoverPublication,Inc.,Mineola,NewYork

2. 3VosD(2009)FiveStepstofacilitatingtheconvergenceofmannedandunmannedaviation.RockwellCollins http://www.webfulfillment.com/cedargraphics/CF/RC/LP/106/images/UAS_eBook09_5mb.pdf. Assessed 05 September 2010

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3. Simulation of a high-agility model airplane in the presence of severe structural damage and failures, and design of a dynamic inversion controller;CEAS Aeronautical Journal;2011-08-27

4. Adaptive Control of a High Agility Model Airplane in the Presence of Severe Structural Damage and Failures;Advances in Aerospace Guidance, Navigation and Control;2011