Control Simulation of Flapping-Wing Micro Aerial Vehicle Based on Multi-Level Optimization Model Predictive Control
Author:
Affiliation:
1. School of Aeronautical and Mechanical Engineering, Changzhou Institute of Technology, Changzhou, China
2. Department of Aeronautics and Astronautics, Zhejiang University, Hangzhou, China
Funder
Natural Science Foundation of Jiangsu Province
Natural Science Foundation of Jiangsu Higher Education Institutions of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx7/6287639/10380310/10471553.pdf?arnumber=10471553
Reference32 articles.
1. Recent Advances in Unmanned Aerial Vehicles: A Review
2. Recent progress in flapping wings for micro aerial vehicle applications
3. Dynamics, stability, and control analyses of flapping wing micro-air vehicles
4. A reciprocating chemical muscle (RCM) for micro air vehicle Entomopter flight;Michelson
5. Non-linear model-free control of flapping wing flying robot using iPID
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