Author:
KOKUME Masanori,UCHIYAMA Kenji
Publisher
Japan Society for Aeronautical and Space Sciences
Reference11 articles.
1. 1) Muraoka, K., Okada, N. and Kubo, D.: Quad Tilt Wing VTOL UAV: Aerodynamic Characteristics and Prototype Flight Test, AIAA, Unmanned… Unlimited Conference, AIAA Paper 2009-1834, 2009.
2. 3) Frank, A., McGrew, J. S., Valenti, M., Levine, D. and How, J. P.: Hover, Transition, and Level Flight Control Design for a Single-Propeller Indoor Airplane, AIAA, Guidance, Navigation and Control Conference and Exhibit, AIAA Paper 2007-6318, 2007.
3. Tail-Sitter Vertical Takeoff and Landing Unmanned Aerial Vehicle: Transitional Flight Analysis
4. 6) Johnson, C. D.: A Family of ``Universal Adaptive Controllers'' for Linear and Nonlinear Plants, Proceedings of the Twentieth Southeastern Symposium on System Theory, 1988, pp. 530-534.
Cited by
2 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Robust Control Design for Quad Tilt-Wing UAV;Aerospace;2018-02-07
2. Control Strategy for Transition Flight of a Fixed-wing UAV;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2014