Experimental Study on the Application of Flat Spin to Vertical Landing of a Fixed-Wing Small UAV

Author:

HIGASHINO Shin-Ichiro1,NAKAMA Kota2,SUMITOMO Yuki2

Affiliation:

1. Department of Aeronautics and Astronautics, Kyushu University

2. Currently, Kawasaki Heavy Industries

Publisher

Japan Society for Aeronautical and Space Sciences

Reference15 articles.

1. 1) Insitu : “Ground Support”, https://www.insitu.com/products (accessed January 5th, 2021)

2. 2) Higashino, S., Hayashi, M., Nagasaki, N., Umemoto, and S., Nishimura, M.: A Balloon-Assisted Gliding UAV for Aerosol Observation in Antarctica, Trans. JSASS Aerospace Tech. Japan, 12, APISAT-2013 (2014), pp. a35-a41. https://doi.org/10.2322/tastj.12.a35

3. 3) Kim, H.J., Kim, M., Lim, H., Park, C., Yoon, S., Lee, D., Choi, H., Oh, G., Park, J., and Kim, Y.: Fully Autonomous Vision-Based Net-Recovery Landing System for a Fixed-Wing UAV, IEEE/ASME Trans. Mechatronics, 18 (2013), pp. 1320-1333.

4. 4) Imgur : “Drone Catcher in Afghanistan”, http://i.imgur.com/AzvsTCH.jpg (accessed November 20th, 2020)

5. 5) Burk, S. M., Jr., Bowman, J. S., Jr. and White, W. L.: Spin-Tunnel Investigation of the Spinning Characteristics of Typical Single-Engine General Aviation Airplane Designs, NASA Technical Paper 1009, 1977.

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