제어로봇시스템학회:학술대회논문집
- 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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- Pages.659-664
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- 1994
Synthesis of a flight control system via nonlinear model matching theory
- Uchikado, Shigeru (Faculty of Science and Engineering, Tokyo Denki Univ.) ;
- Kobayashi, Nobuaki (Kanazawa Institute of Technology) ;
- Osa, Yasuhiro (Department of Mechanical Engineering, Kobe City College of Technology) ;
- Kanai, Kimio (Department of Aerospace Engineering, The National Defence Academy) ;
- Nakamizo, Takayoshi (Department of Information Engineering, The National Defence Academy)
- 발행 : 1994.10.01
초록
In this paper we deal with a synthesis of flight control system via nonlinear model matching theory. First, the longitudinal and lateral-directional equations of aircraft motion an CCV mode are considered except the assumption "variations on steady straight flight due to disturbances are very small". Next, a design method of the dynamic model matching control system based on Hirschorn's Algorithm is proposed to the above nonlinear system. Finally, the proposed control system is applied to the small sized, high speed aircraft, T-2 on CCV mode and numerical simulations are shown to justify the proposed scheme.ed scheme.
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