Crowding and Mutation Improvements in an EA for Flight Control Correction in a Flapping-Wing Vehicle
Author:
Affiliation:
1. University of Cincinnati,Electrical and Computer Enginnering,Cincinnati,OH,USA
2. Autonomous Control Branch, Wright-Patterson Air Force Base,Dayton,OH,USA
3. Purdue University,Computer and Information Technology,West Lafayette,IN
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10371778/10371788/10371914.pdf?arnumber=10371914
Reference14 articles.
1. Dynamics and Control of a Minimally Actuated Biomimetic Vehicle: Part I - Aerodynamic Model
2. Dynamics and Control of a Minimally Actuated Biomimetic Vehicle: Part II-Control
3. Altitude Control of a Single Degree of Freedom Flapping Wing Micro Air Vehicle
4. Model Checking of a Flapping-Wing Mirco-Air-Vehicle Trajectory Tracking Controller Subject to Disturbances
5. The Technology of the Gaps: An Evolvable Hardware Synthesized Oscillator for the Control of a Flapping-Wing Micro Air Vehicle
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