State-Space Modeling and Identification of Delta Wing Vortex-Coupled Roll Dynamics
Author:
Affiliation:
1. Concordia University, Montréal, Québec H3G 1M8, Canada
2. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
3. Defence Research and Development Canada, Valcartier, Québec G3J 1X5, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.23596
Reference49 articles.
1. Robust Vortex Control of a Delta Wing by Distributed Microelectromechanical-Systems Actuators
2. Applications of MEMS devices to delta wing aircraft - From concept development to transonic flight test
3. Micro-actuators for control of delta wing with sharp leading edge
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