Browse "Dept. of Aerospace Engineering(항공우주공학과)" by Author Lee, Yong-In
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| A Practical Optimal Guidance Scheme Under Impact Angle and Terminal Acceleration Constraints Chi, Hyo-Seon; Lee, Yong-In; Lee, Chang-Hun; Choi, Han-Lim, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.22, no.4, pp.923 - 935, 2021-08 |
| Analytic Solutions of Generalized Impact-Angle-Control Guidance Law for First-Order Lag System Lee, Yong-In; Kim, Seung-Hwan; Lee, Jin-Ik; Tahk, Min-Jea, JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.36, no.1, pp.96 - 112, 2013-01 |
| Analytic solutions of optimal angularly constrained guidance for first-order lag system Lee, Yong-In; Kim, Seung-Hwan; Tahk, Min-Jea, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.227, no.G5, pp.827 - 837, 2013-05 |
| Generalized missile guidance law for impact angle control = 일반화된 충돌각 제어 유도법칙 연구link Lee, Yong-In; 이용인; et al, 한국과학기술원, 2012 |
| New Structure for an Aerodynamic Fin Control System for Tail Fin-Controlled STT Missiles Kim, Seung-Hwan; Lee, Yong-In; Tahk, Min-Jea, JOURNAL OF AEROSPACE ENGINEERING, v.24, no.4, pp.505 - 510, 2011-10 |
| Optimality of Linear Time-Varying Guidance for Impact Angle Control Lee, Yong-In; Kim, Seung-Hwan; Tahk, Min-Jea, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.48, no.4, pp.2802 - 2817, 2012-10 |
| 신경회로망을 이용한 BTT 미사일 유도 법칙에 관한 연구 = A study on the guidance law of bank-to-turn missiles using neural networkslink 이용인; Lee, Yong-In; et al, 한국과학기술원, 1995 |
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