Time-Varying Dynamics of a Micro Air Vehicle with Variable-Sweep Morphing
Author:
Affiliation:
1. University of Florida
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6304
Reference14 articles.
1. Internal and External Stability of Linear Time-Varying Systems
2. 3D.T. Grant, M. Abdulrahim and R. Lind, "Flight Dynamics of a Morphing Aircraft utilizing Independent Multiple-Joint Wing Sweep," AIAA-2006-6505.
3. On the poles and zeros of linear, time-varying systems
4. The poles and zeros of a linear time-varying system
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2. Single Network Adaptive Critic (SNAC) Architecture for Optimal Tracking Control of a Morphing Aircraft during a Pull-up Maneuver;AIAA Guidance, Navigation, and Control (GNC) Conference;2013-08-15
3. Single Network Adaptive Critic (SNAC) Design for a Morphing Aircraft;AIAA Guidance, Navigation, and Control Conference;2012-08-13
4. Design and Simulation of a Morphing-Wing Controller with Actuator Loading Penalization;AIAA Atmospheric Flight Mechanics Conference;2011-06-14
5. Modeling of Dynamic Loading of Morphing-Wing Aircraft;Journal of Aircraft;2011-03
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