Modeling and Hover Flight Control of a Micromechanical Flapping-Wing Aircraft Inspired by Wing–Tail Interaction
Author:
Affiliation:
1. School of Automation Science and Electrical Engineering, Beihang University, Beijing, China
2. Research Institute for Frontier Science, Beihang University, Beijing, China
Funder
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering
Link
http://xplorestaging.ieee.org/ielx7/3516/10361845/10089208.pdf?arnumber=10089208
Reference47 articles.
1. Development of the Nano Hummingbird: A Tailless Flapping Wing Micro Air Vehicle
2. Hover flight control of X-shaped flapping wing aircraft considering wing–tail interactions
3. Biologically Inspired Optical-Flow Sensing for Altitude Control of Flapping-Wing Microrobots
4. Quaternion-Based Hybrid Attitude Control for an Under-Actuated Flapping Wing Aerial Vehicle
5. An All Servo-Driven Bird-Like Flapping-Wing Aerial Robot Capable of Autonomous Flight
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