Showing results 2 to 6 of 6
A missile guidance law based on Sontags formula to intercept maneuvering targets Ryoo, Chang-Kyung; Kim, Yoon-Hwan; Tahk, Min-Jea; Choi, Keeyoung, INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, v.5, no.4, pp.397 - 409, 2007-08 |
Guidance synthesis for evasive maneuver of anti-ship missiles = 대함 유도탄의 회피기동을 위한 유도법칙 연구link Kim, Yoon-Hwan; 김윤환; et al, 한국과학기술원, 2009 |
Guidance Synthesis for Evasive Maneuver of Anti-Ship Missiles Against Close-In Weapon Systems Kim, Yoon-Hwan; Ryoo, Chang-Kyung; Tahk, Min-Jea, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.46, no.3, pp.1376 - 1388, 2010-07 |
Optimal UAV formation guidance laws with timing constraint Ryoo, Chang-Kyung; Kim, Yoon-Hwan; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, v.37, no.6, pp.415 - 427, 2006-05 |
Three-Axis Autopilot Design for a High Angle-Of-Attack Missile Using Mixed H-2/H-infinity Control Won, Dae-Yeon; Tahk, Min-Jea; Kim, Yoon-Hwan, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.11, no.2, pp.131 - 135, 2010-06 |
Discover