Longitudinal Linear Parameter Varying Modeling and Simulation of Morphing Aircraft
Author:
Affiliation:
1. School of Aeronautic Science and Engineering, Beihang University, Beijing, People’s Republic of China
2. Department of Chief Aircraft Designer, First Aircraft Design Institute of AVIC, Xi’an, People’s Republic of China, 710089
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031316
Reference21 articles.
1. Mission Effectiveness Comparisons of Morphing and Non-Morphing Vehicles
2. Flight Performance Characteristics of a Tailless Folding Wing Morphing Aircraft
3. The Aircraft Morphing Program
4. Validation of the Lockheed Martin Morphing Concept with Wind Tunnel Testing
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