Verification of Fully Autonomous Flight from Takeoff to Landing of a Low-Speed Model Airplane with Application to a Small Unmanned Supersonic Airplane

Author:

UEBA Masazumi1,KAMATA Tomohiro1,NAKAJIMA Sakurako1,MAEDA Yosuke1

Affiliation:

1. Graduate School, Muroran Institute of Technology

Publisher

Japan Society for Aeronautical and Space Sciences

Reference17 articles.

1. 1) Maki, M., Takeda, S., and Ishikawa, K.: Automatic Recovery System for Fixed-Wing Mini-UAV Aiming Disaster Monitoring Design Concept and Simulations-, Trans. on the SICE Industrial Application, 10 (2011), pp. 123–131 (in Japanese).

2. 2) Harada, K., Sasa, S., Ishikawa, K., Kohno, T., Hosokawa, M., and Tamura, H.: Research and Development of Disaster Monitoring UAV System- System Concept and Demonstration Test -, Proceedings of the 51st Aircraft Symposium, Takamatsu, Japan, 2F06, 2013 (in Japanese).

3. 3) Maki, M. and Ishikawa, K.: Full Automatization of A DisasterMonitoring System Using A Fixed-Wing Mini UAV - Flight Control System Design, Development and Demonstration -, Proceedings of the 51st Aircraft Symposium, Takamatsu, Japan, 2F08, 2013 (in Japanese).

4. 4) Miyazawa, Y., Motoda, T., Izumi, T., and Hata, T.: Longitudinal Landing Control Law for an Autonomous Reentry Vehicle, J. Guidance, Control, and Dynamics, 22 (1999), pp. 791–800.

5. 5) Iigo, R. and Tanabe, S.: Full Automatic Landing System and LongDistance Flight of the Fixed-Wing UAV, Proceedings of the 50th automatic control rengo kouenkai, 506, Yokohama, Japan, pp. 340–342, 2007 (in Japanese).

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