Difficulty of Controlling a Flapping-wing Aircraft Compared to a Rotary-wing Aircraft
Author:
Affiliation:
1. Department of Aerospace Engineering, Nagoya University
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/66/4/66_T-22-43/_pdf
Reference23 articles.
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2. 2) Chand, A. N., Kawanishi, M., and Narikiyo, T.: Adaptive Pole Placement Pitch Angle Control of a Flapping-wing Flying Robot, Adv. Robot., 30, 16 (2016), pp. 1039–1049. doi: 10.1080/01691864.2016.1196609
3. 3) Zuo, D., Chen, W., Peng, S., and Zhang, W.: Modeling and Simulation Study of an Insect-like Flapping-wing Micro Aerial Vehicle, Adv. Robot., 20, 7 (2006), pp. 807–824. doi: 10.1163/156855306777681393
4. 4) Lu, G., Yan, J., Zhang, Z., Shi, J., and Yan, Y.: Dissection of a Flexible Wing’s Performance for Insect-inspired Flapping-wing Micro Air Vehicles, Adv. Robot., 26, 5-6 (2012), pp. 409–435. doi: 10.1163/156855311X617443
5. 5) Hamamoto, M., Ohta, Y., Hara, K., and Hisada, T.: Basic Design Strategy for Stiffness Distribution on a Dragonfly-mimicking Wing for a Flapping Micro Aerial Vehicle, Adv. Robot., 24, 5-6 (2010), pp. 861–877. doi: 10.1163/016918610X493642
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