제어로봇시스템학회:학술대회논문집
- 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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- Pages.653-658
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- 1994
On the 3-dimensional low speed yo-yo maneuver
- Takano, Hiroyuki (Dept. of Aerospace Engineering, National Defense Academy, Japan) ;
- Sato, Masaya (Dept. of Aerospace Engineering, National Defense Academy, Japan) ;
- Baba, Yoriaki (Dept. of Aerospace Engineering, National Defense Academy, Japan)
- 발행 : 1994.10.01
초록
This paper presents numerical analyses of the low speed yo-yo maneuver of an aircraft to determine controls of thrust, bank-angle and angle-of-attack in the subsonic region in terms of the optimal control theory. Minimum-time flight paths are numerically calculated to overtake an opponent aircraft flying in some steady-state level turnings under several assumptions: both of aircraft are point masses and maneuver in the 3-Dimensional space. Their weights are considered constant in the maneuver. As a result of the analyses, the effectiveness of the low speed yo-yo maneuver is shown.
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