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| NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
|---|---|
| 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 |