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| NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
|---|---|
| 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 | |
| Missile acceleration controller design using proportional-integral and non-linear dynamic control design method Kim, Seung-Hwan; Tahk, Min-Jea, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.226, no.G8, pp.882 - 897, 2012-08 | |
| 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 | |
| Aerodynamic coupling model development and autopilot design for highly manoeuvring skid-to-turn missiles Kim, Seung-Hwan; Kim, Y-S; Lee, Y-I; Tahk, Min-Jea, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.226, no.G5, pp.498 - 509, 2012-05 | |
| 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 | |
| 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 | |
| Experimental Study on Integrated Servo Control for Canard-Controlled Missiles Kim, Sang Hwa; Tahk, Min-Jea; Lee, Ha-Jun; Kim, Seung-Hwan, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.52, no.3, pp.1467 - U569, 2016-06 |
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