Simulation of Individual Blade Control Helicopter for Analysis of Fault Tolerance Capabilities-Reference-Cited by-同舟云学术

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Simulation of Individual Blade Control Helicopter for Analysis of Fault Tolerance Capabilities

Published:2010-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Modeling and Simulation Technologies Conference
language:
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Author:

Tamayo Sergio¹,Perhinschi Mario¹

Affiliation:

1. West Virginia University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-7789

Reference20 articles.

1. 1Straub, F. K. "A Feasibility Study of Using Smart Materials for Rotorcraft", Smart Materials and Structures, Vol 5 No 1,1995.

2. Swashplateless Helicopter Rotor with Trailing-Edge Flaps

3. 5Zimmer, H. "Helicopter Rotor Blade Control", Dornier GmbH, United States Patent, Patent # 4799859, January1989.

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