Low Cost Flight-Test Platform to Demonstrate Flight Dynamics Concepts using Frequency-Domain System Identification Methods-Reference-Cited by-同舟云学术

Low Cost Flight-Test Platform to Demonstrate Flight Dynamics Concepts using Frequency-Domain System Identification Methods

Published:2013-08-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics (AFM) Conference
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Author:

Woodrow Paul¹,Tischler Mark²,Mendoza Gonzalo³,Hagerott Steven G.³,Hunter Jeanine¹

Affiliation:

1. San Jose State University

2. Army Aviation and Missile Research Development and Engineering Center

3. Cessna Aircraft Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4739

Reference11 articles.

1. 3Salluce, D. N. "ComprehensiveSystemIdentification ofDucted Fan UAVS",Ph.D. Thesis, AerospaceEngineeringDept.CaliforniaPolytechnicStateUniv., San Luis Obispo,2004.

2. 4Carnduff, S. D. "System Identification of Unmanned Aerial Vehicles," Ph.D. Thesis,Cranfield University, Cranfield, Bedfordshire, 2008.

3. 13Gracey, W. "The Experimental Determination of the Moments of Inertia of Airplanes by a Simplified Compound-PendulumMethod,"NACATN-1629, 1948.

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