
Insect-Inspired Flapping-Wing Robots
Description
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Features:
Describes the latest breakthrough and technology in the design, fabrication, and control of the insect-like flapping-wing robots
Addresses the challenges in this field, such as power efficiency and flight stability, and provides a roadmap for future research
Showcases the potential applications of these robots
Describes unsteady blade element theory as a simpler method for aerodynamic force estimation compared to the CFD
Details two different designs of control moment generators that are essential for attitude control
This book is aimed at graduate students and researchers in robotics, aerospace, and mechanical engineering.
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Persons
Hoang-Vu Phan received MS and PhD degrees in biomimetics and intelligent microsystems from Konkuk University, Seoul, South Korea in 2012 and 2017, respectively, and BE degree in aerospace engineering from the Vietnam National University - Ho Chi Minh city University of Technology, Ho Chi Minh, Vietnam in 2010. He is currently an Assistant Professor in Aerospace Engineering at the University of Nevada, Reno, USA. From 2021 to 2025, he was a Senior Postdoctoral Scientist at the Swiss Federal Institute of Technology Lausanne (EPFL), Switzerland. Prior to joining EPFL, he was a non-tenure-track Assistant Professor in the Department of Smart Vehicle Engineering, Konkuk University, Seoul, Korea (2017-2021). His research interests include biologically inspired aerial robotics, multimodal locomotion, flapping-wing flight, and biomechanics of animal flight. He has published more than 30 papers in prestigious journals across various disciplines. He has moreover presented his work at numerous renowned international conferences. Dr. Phan currently serves on the editorial boards of npj Robotics (Nature Portfolio), International Journal of Micro Air Vehicles, and Aerospace.
Content
2. Design and fabrication
3. Measurements
4. Prediction of aerodynamic forces
5. System integration and controlled flight
6. Flying like a beetle
7. Toward flapping flight on Mars
8. Concluding remarks
Appendix
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