Showing results 120 to 179 of 488
Capturability analysis of PN laws using Lyapunov stability theory Ryoo, C.-K.; Kim, Y.-H.; Tahk, Min-Jea, Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference, v.1, pp.722 - 734, 2004-08-16 |
Capturability of 3D PPN Against Lower-Speed Maneuvering Target for Homing Phase Li, Ke-Bo; Shin, Hyo-Sang; Tsourdos, Antonios; Tahk, Min-Jea, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.56, no.1, pp.711 - 722, 2020-02 |
Capturability of 3D RTPN Against True-Arbitrarily Maneuvering Target with Maneuverability Limitation Li, Ke-Bo; Bai, Zhi-Hui; Shin, Hyo-Sang; Tsourdos, Antonios; Tahk, Min-Jea, International Conference on Guidance, Navigation and Control, ICGNC 2020, pp.4511 - 4528, Springer Science and Business Media Deutschland GmbH, 2020-10 |
Capturability of 3D RTPN guidance law against true-arbitrarily maneuvering target with maneuverability limitation LI, Kebo; Bai, Zhihui; Shin, Hyo-Sang; Tsourdos, Antonios; Tahk, Min-Jea, CHINESE JOURNAL OF AERONAUTICS, v.35, no.7, pp.75 - 90, 2022-07 |
Cascade-type guidance law design for multiple-UAV formation keeping No, Tae Soo; Kim, Youdan; Tahk, Min-Jea; Jeon, Gyeong-Eon, AEROSPACE SCIENCE AND TECHNOLOGY, v.15, no.6, pp.431 - 439, 2011-09 |
Closed-form optimal guidance law for missiles of time-varying velocity Cho, HJ; Ryoo, CK; Tahk, Min-Jea, JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.19, no.5, pp.1017 - 1022, 1996-09 |
Closed-form solutions of optimal guidance with terminal impact angle constraint Ryoo, C.-K.; Cho, H.; Tahk, Min-Jea, Proceedings of 2003 IEEE Conference on Control Applications, pp.504 - 509, IEEE, 2003-06-23 |
Co-evolutioanry methods for trajectory optimization of space launch vehicles Woo, H.W.; Roh, W.R.; Kim, Y.; Tahk, Min-Jea, JSASS Aircraft Symposium, JSASS, 1999-10 |
Co-Evolution and Numerical Optimization (invited lecture) Tahk, Min-Jea, ICCAS 2004, 2004-08 |
co-evolution for engineering optimization problems: minimax design and constrained optimization Tahk, Min-Jea, JSASS Aircraft Symposium, JSASS, 1998-10 |
Co-evolutionary approaches to pursuit-evasion games (invited paper) Tahk, Min-Jea; Choi, H.L., JSASS Aircarft Symposium, JSASS, 2003-10 |
Co-evolutionary computation for constrained min-max problems Kim, J.G.; Tahk, Min-Jea, JSASS Aircraft Symposium, JSASS, 2000-10 |
Co-evolutionary computation for constrained min-max prolems and its application for pursuit-evasion games Kim, J.G.; Tahk, Min-Jea, Congress on Evolutionary Computation, 2001-05 |
A co-evolutionary method for pursuit-evasion games with non-zero lethal radii Choi, Han-Lim; Ryu, Hyeok; Tahk, Min-Jea; Bang, Hyochoong, Engineering Optimization, Vol 36, No.1, pp.19-36, 2004-02 |
Co-evolutionary optimization of three-dimensional target evasive maneuver against a proportionally guided missile Choi, Han-Lim; Bang, Hyochoong; Tahk, Min-Jea, Congress on Evolutionary Computation, CEC, 2001-05 |
Coevolutionary approaches to structural optimization Tahk, Min-Jea; Kim, Y; Nam, C, AIAA JOURNAL, v.37, no.8, pp.1019 - 1021, 1999-08 |
Coevolutionary augmented Lagrangian methods for constrained optimization Tahk, Min-Jea; Sun, BC, IEEE TRANSACTIONS ON EVOLUTIONARY COMPUTATION, v.4, no.2, pp.114 - 124, 2000-07 |
Command Shaping Optimal Guidance Laws Against High-Speed Incoming Targets Ryu, Moo Yong; Lee, Chang-Hun; Tahk, Min-Jea, JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.38, no.10, pp.2025 - 2032, 2015-10 |
Conceptual Design of a Multi-Rotor Unmanned Aerial Vehicle Based on an Axiomatic Design Yoo, Dong-Wan; Won, Dae-Yeon; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.11, no.2, pp.126 - 130, 2010-06 |
Constrained trajectory optimization for lunar landing during the powered descent phase Park, B.-G.; Sang, D.; Tahk, Min-Jea, ICROS-SICE International Joint Conference 2009, ICCAS-SICE 2009, pp.4226 - 4231, 2009-08-18 |
Control design of spinning rockets based on co-evolutionary optimization Lee, HI; Sun, BC; Tahk, Min-Jea; Lee, H, CONTROL ENGINEERING PRACTICE, v.9, no.2, pp.149 - 157, 2001-02 |
Control Input Blending Logic with Aerodynamic Control and Reaction Jet Control Seo, Min Guk; Lee, Chang-Hun; Tahk, Min-Jea; Lee, Jin Ik; 전병을, 29th Congress of the International Council of the Aeronautical Sciences, International Council of the Aeronautical Sciences, 2014-09 |
Control system design and aggressive maneuver method for a quad-rotor UAV = 쿼드-로터 무인항공기의 제어시스템 설계 및 고기동 기법 연구link Lee, Byung-Yoon; 이병윤; et al, 한국과학기술원, 2013 |
Control system design and vision based collision avoidance of multi-rotor UAV = 멀티-로터 무인항공기의 제어시스템 설계 및 영상 기반 충돌회피 기법 연구link Yoo, Dong-Wan; 유동완; et al, 한국과학기술원, 2011 |
Control system design and vision based collision avoidance of multi-rotor UAV = 멀티-로터 무인항공기의 제어시스템 설계 및 영상 기반 충돌회피 기법 연구link Yoo, Dong-Wan; 유동완; et al, 한국과학기술원, 2011 |
Control-Oriented Model for Intake Shock Position Dynamics in Ramjet Engine Park, Ik-Soo; Kim, Sun-Kyoung; Yeom, Hyo-Won; Sung, Hong-Gye; Park, Jung-Woo; Tahk, Min-Jea, JOURNAL OF PROPULSION AND POWER, v.27, no.2, pp.499 - 502, 2011-04 |
Controller reduction using a new invariant set Sun, BC; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF CONTROL, v.70, no.3, pp.447 - 467, 1998-06 |
Convex Programming-based Optimal Three-Dimensional Mid-course Guidance with Lossless Convexification Jung, Cheol-Goo; Lee, Chang-Hun; Tahk, Min-Jea, 33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022, International Council of the Aeronautical Sciences (ICAS), 2022-09-08 |
Coprime factorization controller reduction using a new set of invariants = 새로운 불변항을 이용한 소인수분해 제어기 축소link Sun, Byung-Chan; 선병찬; et al, 한국과학기술원, 1997 |
Covariance analysis on spacecraft attitude control system Kim, Y.-H.; Park, Y.; Bang, H.; Tahk, Min-Jea, 2003 IEEE International Conference on Control Applications, v.1, pp.480 - 485, IEEE, 2003-06-23 |
Decentralized target localization by multiple missiles Sang, Daekyu; Ryoo, Chang-Kyung; Kim, Hyoun Jin; Tahk, Min-Jea, 2009 10th European Control Conference, ECC 2009, pp.132 - 137, Institute of Electrical and Electronics Engineers Inc., 2009-08 |
Decorrelated Debiased Converted Measurement Kalman Filter for Phased Array Radar Tracking System Cho, Min-Hyun; Tahk, Min-Jea, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.58, no.1, pp.581 - 595, 2022-02 |
Design and analysis of optimal controller for fuzzy systems with input constraint Park, Y; Tahk, Min-Jea; Bang, Hyochoong, IEEE TRANSACTIONS ON FUZZY SYSTEMS, v.12, no.6, pp.766 - 779, 2004-12 |
Design and control of a quad-rotor UAV = 쿼드-로터 무인항공기 설계 및 제어기법 연구link Choi, Dae-Hyung; 최대형; et al, 한국과학기술원, 2009 |
Design of generalized Time-to-go polynomial guidance law with terminal constraints = 종말 구속조건을 고려한 일반화된 Time-to-go 다항식 유도법칙의 설계link Kim, Tae-Hun; 김태훈; et al, 한국과학기술원, 2012 |
Design of guidance law for passive homing missile using sliding mode control Lee, C.-H.; Kim, T.-H.; Tahk, Min-Jea, International Conference on Control, Automation and Systems, ICCAS 2010, pp.2380 - 2385, 2010-10-27 |
Design of impact angle control guidance laws via high-performance sliding mode control Lee, Chang-Hun; Kim, Tae-Hun; Tahk, Min-Jea, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.227, no.G2, pp.235 - 253, 2013-02 |
Design of missile autopilot using PI and approximate feedback linearization control with time-delay adaptation scheme Lee, Chang-Hun; Lee, Yong-Woo; Jun, Byung-Eul; Tahk, Min-Jea, 13th European Control Conference, ECC 2014, pp.2762 - 2767, Institute of Electrical and Electronics Engineers Inc., 2014-06 |
Design of robust sliding mode controllers for missiles with unmatched uncertainty = 부정합 불확실성을 갖는 유도탄에 대한 강인한 슬라이딩 모드 제어기 설계link Hwang, Donghyeok; Tahk, Min-Jea; et al, 한국과학기술원, 2019 |
Development of Flight Control System and Troubleshooting on Flight Test of a Tilt-Rotor Unmanned Aerial Vehicle Kang, Youngshin; Park, Bum-Jin; Cho, Am; Yoo, Chang-Sun; Koo, Sam-Ok; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.17, no.1, pp.120 - 131, 2016-03 |
Differential Game Based Air Combat Maneuver Generation Using Scoring Function Matrix Park, Hyunju; Lee, Byung Yoon; Tahk, Min-Jea; Yoo, Dong-Wan, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.17, no.2, pp.204 - 213, 2016-06 |
Direct trajectory optimization of a soft lunar landing considering a landing site Park, B.-G.; Sang, D.; Tahk, Min-Jea, 60th International Astronautical Congress 2009, IAC 2009, v.6, pp.4413 - 4423, 2009-10-12 |
Dynamic modeling and control system design for a quad-rotor UAV = 쿼드 로터 무인항공기 동역학 모델링 및 제어시스템 설계 연구link Won, Dae-Yeon; 원대연; et al, 한국과학기술원, 2008 |
Dynamic modeling and control system design for tri-rotor UAV Yoo, D.-W.; Oh, H.-D.; Won, D.-Y.; Tahk, Min-Jea, 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010, pp.762 - 767, 2010-06-08 |
Dynamic Modeling and Stabilization Techniques for Tri-Rotor Unmanned Aerial Vehicles Yoo, Dong-Wan; Oh, Hyon-Dong; Won, Dae-Yeon; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.11, no.3, pp.167 - 174, 2010-09 |
Dynamic Stiffness Transfer Function of an Electromechanical Actuator Using System Identification Kim, S.H.; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.19, no.1, pp.208 - 216, 2018-03 |
Dynamics modeling and robust controller design of the multi-UAV transportation system Lee, Hae-In; Lee, Byung Yoon; Yoo, Dong Wan; Moon, Gun-Hee; Tahk, Min-Jea, 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, International Council of the Aeronautical Sciences, 2014-09 |
Effects of side jet on pursuit-evasion games Lee, S.-J.; Lee, J.-I.; Tahk, Min-Jea, Proceedings of 2003 IEEE Conference on Control Applications, 2003, pp.498 - 503, IEEE, 2003-06-23 |
Effects of Time-to-Go Errors on Performance of Optimal Guidance Laws Lee, Chang-Hun; Kim, Tae-Hun; Tahk, Min-Jea, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.51, no.4, pp.3270 - 3281, 2015-10 |
Effects of time-to-go freezing on PN guidance loop stability Rew, D.Y.; Tahk, Min-Jea, Korea Automatic Control Conference, 1995-10 |
End game 의 수치해법적 연구 = Numerical methods for end game analysislink 황태원; Hwang, Tae-Won; et al, 한국과학기술원, 1996 |
Energy Optimal Waypoint Guidance Synthesis for Antiship Missiles Ryoo, Chang-Kyung; Shin, Hyo-Sang; Tahk, Min-Jea, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.46, no.1, pp.80 - 95, 2010-01 |
Evolution-based hessian approximation for hybrid numerical optimization methods = 하이브리드 수치최적화 기법을 위한 진화기반 헤시안 추정link Park, Moon-Su; 박문수; et al, 한국과학기술원, 2009 |
Evolutionary optimized pitching motion control for F-16 aircraft Lee, Kang-Hee; Lee, Chi-Ho; Kim, Jong-Hwan; Choi, Han-Lim; Tahk, Min-Jea, IEEE Congress on Evolutionary Computation, 2002, pp.1940 - 1945, IEEE, 2002-05 |
Experimental Framework for Controller Design of a Rotorcraft Unmanned aerial Vehicle Using Multi-Camera System Oh, Hyondong; Won, Dae-Yeon; Huh, Sung-Sik; Shim, David Hyunchul; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL & SPACE SCIENCES, v.11, no.2, pp.69 - 79, 2010-06 |
Experimental study on dynamic stiffness and servo control of missile actuation systems = 유도탄 구동장치의 동강성 및 서보 제어에 대한 실험 연구link Kim, Sang Hwa; 김상화; et al, 한국과학기술원, 2016 |
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 |
Extended Kalman filter design using bearing and time-to-go measurement for a homing missile guidance Shim, Sang-Wook; Park, Bong-Gyun; Jeon, Byoung-Ju; Tahk, Min-Jea; Kwon, Hyuck Hoon, 29th Congress of the International Council of the Aeronautical Sciences, International Council of the Aeronautical Sciences, 2014-09-09 |
Fast Adaptive Guidance Against Highly Maneuvering Targets Cho, Dongsoo; Kim, Hyun Jin; Tahk, Min-Jea, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.52, no.2, pp.671 - 680, 2016-04 |
Fast Trajectory Optimization Using Sequential Convex Method for Guided Missiles Roh, Heekun; Oh, Young-Jae; Tahk, Min-Jea; Lee, Chang-Hun, 5th CEAS conference on Guidance, Navigation and Control (EuroGNC19), Council of European Aerospace Societies (CEAS), 2019-04-04 |
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