Air Combat Guidance Law for an UCAV

Author:

Baba Yoriaki1,Takano Hiroyuki1,Miyamoto Seiji2,Ono Kenjiro2

Affiliation:

1. National Defense Academy

2. Fujitsu Limited

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 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. Effects of Propulsion System Operation on Military Aircraft Survivability;Journal of Aircraft;2019-11

2. A Study on the Dynamic Inversion Method with nonlinear function considering saturation;AIAA Guidance, Navigation, and Control Conference;2010-06-26

3. A Study on a Velocity Control System Design Using the Dynamic Inversion Method;AIAA Guidance, Navigation, and Control Conference;2010-06-26

4. Advanced Pure Pursuit Guidance via Sliding Mode Approach for Chase UAV;AIAA Guidance, Navigation, and Control Conference;2009-06-14

5. Velocity Control System Design for Leader-Following UAV Using Dynamic Inversion;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2009

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