Browse "Dept. of Aerospace Engineering(항공우주공학과)" by Author Tahk, Min-Jea
Showing results 330 to 389 of 488
| Parameter optimization of multistage missile for terminal velocity maximization Lee, Jun-Yong; Hong, Seong-Min; Kim, Young-Won; Tahk, Min-Jea, 7th Asia-Pacific International Symposium on Aerospace Technology, APISAT 2015, pp.276 - 282, Asia-Pacific International Symposium on Aerospace Technology (APISAT), 2015-11 |
| Parameter robust control design using bimatrix co-evolution algorithms Hur, J; Lee, H; Tahk, Min-Jea, ENGINEERING OPTIMIZATION, v.35, no.4, pp.417 - 426, 2003-08 |
| PARAMETER ROBUST LINEAR-QUADRATIC-GAUSSIAN DESIGN SYNTHESIS WITH FLEXIBLE STRUCTURE CONTROL APPLICATIONS Tahk, Min-Jea; SPEYER, JL, JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.12, no.4, pp.460 - 468, 1989-07 |
| Parameter-robust control design using co-evolution Hur, J.; Tahk, Min-Jea, JSASS Aircraft Symposium, JSASS, 1998-10 |
| Parameter-robust linear quadratic Gaussian technique for multi-agent slung load transportation Lee, Hae-In; Yoo, Dong-Wan; Lee, Byung Yoon; Moon, Gun-Hee; Lee, Dong-Yeon; Tahk, Min-Jea; Shin, Hyo-Sang, AEROSPACE SCIENCE AND TECHNOLOGY, v.71, pp.119 - 127, 2017-12 |
| Particle swarm optimization for airship controller design Park, C.S.; Bang, Hyochoong; Tahk, Min-Jea, 16th JSASS Aircraft Symposium, pp.137 - 140, JSASS, 2002-10 |
| PASSIVE HOMING MISSILE GUIDANCE LAW BASED ON NEW TARGET MANEUVER MODELS Speyer, Jason L.; Kim, Kevin D.; Tahk, Min-Jea, JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.13, no.5, pp.803 - 812, 1990-09 |
| Pendulum Modeling of Sloshing Motion Using Particle Swarm Optimization Lee, Dong-Yeon; Cho, Min-Hyun; Choi, Han-Lim; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.20, no.1, pp.172 - 182, 2019-03 |
| Perch Landing Assisted by Thruster (PLAT): Concept and Trajectory Optimization Tahk, Min-Jea; Han, Seungyeop; Lee, Byung Yoon; Ahn, Jaemyung, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.17, no.3, pp.378 - 390, 2016-09 |
| Performance Analysis of an Integrated Navigation of an Airborne AESA Radar Lee, Dong-Yeon; Kwon, Hyeokjoon; Lee, Donguk; Lee, Haemin; Jung, Youngkwang; Jeong, Jaehyeon; Park, Sanggyu; et al, JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, v.49, no.4, pp.281 - 290, 2021-04 |
| Performance analysis of attitude-hold proportional navigation guidance for high-altitude defense missiles = 고고도 방어 유도탄의 자세유지 비례항법 성능 분석link Yoon, SungJin; Tahk, Min-Jea; et al, 한국과학기술원, 2019 |
| Performance Analysis of Modified Gain Pseudo-Measurement Filter for Ballistic Target Tracking Lee, Dong-Yeon; Hong, Seong-Min; Tahk, Min-Jea, 21st International-Federation-of-Automatic-Control (IFAC) Symposium on Automatic Control in Aerospace (ACA), pp.7 - 12, ELSEVIER, 2019-08 |
| Performance analysis of pursuit-evasion game based guidance laws Kim, Young-Sam; Kim, Tae-Hun; Tahk, Min-Jea; Ryu, Hyeok, 2007 9th European Control Conference, ECC 2007, pp.1798 - 1804, Institute of Electrical and Electronics Engineers Inc., 2007-07 |
| Performance characteristics of linear optimal guidance laws for varying velocity missiles Ryoo, C.K.; Cho, H.J.; Tahk, Min-Jea, 2nd Asian Control Conference, 1997-07 |
| Performance comparison of the optimal guidance law and proportional navigation for missile homing Tahk, Min-Jea; Park, B.K.; Hwang, I.S., 32st SICE Annual Conference, 1993-08 |
| Performance comparison of three different types of attitude control systems of the quad-rotor UAV to perform flip maneuver Lee, Byung Yoon; Yoo, Dong Wan; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.14, no.1, pp.58 - 66, 2013-03 |
| Performance of 3-D PPN Against Arbitrarily 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.5, pp.3878 - 3891, 2020-10 |
| Plant inversion control of tail-controlled missiles Ryu, J.H.; Park, C.S.; Tahk, Min-Jea, AIAA Conference on Guidance, Navigation, and Control, AIAA, 1997-08 |
| Polynomial Guidance Laws Considering Terminal Impact Angle and Acceleration Constraints Lee, Chang-Hun; Kim, Tae-Hun; Tahk, Min-Jea; Whang, Ick-Ho, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.49, no.1, pp.74 - 92, 2013-01 |
| POSTFLIGHT DATA-REDUCTION TECHNIQUES FOR HOVERED KINETIC-ENERGY WEAPONS Tahk, Min-Jea; TRIKAS, T; WALLACE, B, JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.14, no.5, pp.872 - 877, 1991-09 |
| Practical dual-control guidance of passive homing missiles = 수동형 호밍유도탄의 실용적인 이중제어 유도기법link Lee, Ho-Il; 이호일; et al, 한국과학기술원, 2001 |
| Practical dual-control guidance using adaptive intermittent maneuver strategy Lee, HI; Tahk, Min-Jea; Sun, BC, JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.24, no.5, pp.1009 - 1015, 2001-09 |
| Practical time-to-go estimation methods for optimal guidance Ryoo, C.K.; Tahk, M.J.; Tahk, Min-Jea, AIAA Conference on Guidance, Navigation, and Control, AIAA, 1999-08 |
| Prediction based terminal velocity control guidance law = 예측 기반 종말속도제어 유도 기법link Moon, Gun-Hee; Tahk, Min-Jea; et al, 한국과학기술원, 2019 |
| Prediction of clinical pregnancy in IVF-ET cycle using neural network Kang, I.S.; Tahk, Min-Jea, 16th World Congress on Fertility and Sterility & the 54th Annual Meeting of the Amer. Soc. for Reproductive Medicine Annual Meeting, 1998-10 |
| Pseudospectral method-based safe motion planning for quadrotors in a cluttered environment Han, Juyeop; Tahk, Min-Jea; Choi, Han-Lim, AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022, American Institute of Aeronautics and Astronautics Inc, AIAA, 2022-01 |
| Pursuit-Based Long-Range Air-to-Air Missile Midcourse Guidance Robust to Changes in the Predicted Impact Point Shin, Minjae; Tahk, Min-Jea; Kim, Boseok; Lee, Chang-Hun, 34th Congress of the International Council of the Aeronautical Sciences, ICAS 2024, International Council of the Aeronautical Sciences (ICAS), 2024-09-11 |
| Radome aberration estimation and target tracking with line-of-sight angle measurement = 시선각 측정을 통한 레이돔 오차 추정 및 표적 추적 기법 연구link Seo, Min-Guk; 서민국; et al, 한국과학기술원, 2014 |
| Radome Aberration Estimation using Bearing-Only Measurement Seo, Min Guk; Tahk, Min-Jea, 2013 Asia-Pacific International Symposium on Aerospace Technology, Japan Society for Aeronautical and Space Science, 2013-11 |
| Range-to-Go Weighted Optimal Guidance With Impact Angle Constraint and Seeker's Look Angle Limits Park, Bong-Gyun; Kim, Tae-Hun; Tahk, Min-Jea, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.52, no.3, pp.1241 - 1256, 2016-06 |
| Real time path-planning algorithm and guidance logic for glider bomb Lee, C.-H.; Kim, T.-H.; Tahk, Min-Jea, ICROS-SICE International Joint Conference 2009, ICCAS-SICE 2009, pp.3640 - 3645, 2009-08-18 |
| Real-time midcourse guidance robust to missile launch conditions Song, E.J.; Tahk, Min-Jea, IFAC Symposium on Automatic Control in Aerospace, IFAC, 1998-08 |
| Real-time midcourse guidance with intercept point prediction Song, EJ; Tahk, Min-Jea, CONTROL ENGINEERING PRACTICE, v.6, no.8, pp.957 - 967, 1998-08 |
| Real-time midcourse missile guidance robust against launch conditions Song, EJ; Tahk, Min-Jea, CONTROL ENGINEERING PRACTICE, v.7, no.4, pp.507 - 515, 1999-04 |
| Real-time missile midcourse guidance = 미사일 중기유도법칙의 실시간 구현에 관한 연구link Song, Eun-Jung; 송은정; et al, 한국과학기술원, 2000 |
| Real-time neural-network midcourse guidance Song, EJ; Tahk, Min-Jea, CONTROL ENGINEERING PRACTICE, v.9, no.10, pp.1145 - 1154, 2001-10 |
| Real-time trajectory optimization of UAV using sequential convex programming = 순차 컨벡스 계획법을 이용한 무인항공기의 실시간 궤적 최적화link Oh, Young-Jae; Tahk, Min-Jea; et al, 한국과학기술원, 2019 |
| Reconstruction of high-frequency lunar digital elevation model using shape from shading Cho, M.-H.; Tahk, Min-Jea, INCAS Bulletin, v.10, no.1, pp.5 - 12, 2018 |
| Recursive time-to-go estimation for homing guidance missiles Tahk, Min-Jea; Ryoo, CK; Cho, H, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.38, no.1, pp.13 - 24, 2002-01 |
| Reliable and Computational Effective On-Board Stationkeeping System for Geostationary Satellites Park, B.K.; Choi, S.B.; Tahk, Min-Jea, , 2003 |
| Retrofit Flight Control Using an Adaptive Chebyshev Function Approximator Shin, Sung-Sik; Min, Byoung-Mun; Tahk, Min-Jea, JOURNAL OF AEROSPACE ENGINEERING, v.26, no.4, pp.735 - 749, 2013-10 |
| Retrofit flight control using an adaptive chebyshev function approximator = 적응 체비셰프 함수근사기를 이용한 개선 비행제어link Shin, Sung-Sik; 신성식; et al, 한국과학기술원, 2011 |
| Robust attitude stabilization of spacecraft using minimal kinematic parameters Park, Y.; Tahk, Min-Jea, 2001 IEEE International Conference on Robotics and Automation (ICRA), pp.1621 - 1626, IEEE, 2001-05-21 |
| Robust controller design for spinning rockets Sun, Byung-Chan; Ryu, Jin-Hoon; Tahk, Min-Jea, Proceedings of the 1996 35th SICE Annual Conference, SICE'96, pp.1325 - 1329, 1996-07-24 |
| Robust disturbance decoupling Tahk, Min-Jea; Speyer, J.L., 12th International Association for Mathematics and Computers in Simulation (IMACS) World Congress, 1988-07 |
| Robust flight control design using co-evolution with considerations of design constraints Hur, J.; Tahk, Min-Jea, 3rd Asian Control Conference, 2000-07 |
| Robust gain scheduling method based on fuzzy logic control and LMI methods = 퍼지논리제어와 LMI 기법을 이용한 강인 게인 스케쥴링link Koo, Kuen-Mo; 구근모; et al, 한국과학기술원, 2001 |
| Robust gain-scheduling technique for an agile missile subject to mass variation Won, D.-Y.; Tahk, Min-Jea; Kim, K.-Y., International Conference on Control, Automation and Systems, ICCAS 2010, pp.2119 - 2123, 2010-10-27 |
| Robust roll-pitch-yaw integrated autopilot for a high angle-of-attack missile Kang, S.; Kim, H.J.; Won, D.; Tahk, Min-Jea; Lee, J.-I.; Jun, B.-E., AIAA Guidance, Navigation and Control Conference and Exhibit, 2008-08-18 |
| Robust Stabilization Technique for the Leader Steering Slung-Load System/Using Sliding Mode Control Oh, Hyun-Shik; Tahk, Min-Jea; Yoo, Dong-Wan; Lee, Byung-Yoon, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.19, no.4, pp.932 - 944, 2018-12 |
| Robustness Characteristics of Missile Autopilot Systems Based on Feedback Linearization Tahk, Min-Jea, JSASS Aircraft Symposium, JSASS, 1990-11 |
| Robustness Improvement for a Three-Loop Missile Autopilot Using Discontinuous State Feedback Hwang, Donghyeok; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.19, no.3, pp.661 - 674, 2018-09 |
| Roll-pitch-yaw integrated mu-synthesis for high angle-of-attack missiles Choi, Byunghun; Kang, Seonhyeok; Kim, H. Jin; Jun, Byung-Eul; Lee, Jin-Ik; Tahk, Min-Jea; Park, Changhan, AEROSPACE SCIENCE AND TECHNOLOGY, v.23, no.1, pp.270 - 279, 2012-12 |
| Roll-Pitch-Yaw Integrated Robust Autopilot Design for a High Angle-of-Attack Missile Kang, Seonhyeok; Kim, H. Jin; Lee, Jin-Ik; Jun, Byung-Eul; Tahk, Min-Jea, JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.32, no.5, pp.1622 - 1628, 2009-09 |
| Satellite attitude stabilization using solar radiation pressure and magnetotorquer Kumar, K. D.; Tahk, Min-Jea; Bang, Hyochoong, CONTROL ENGINEERING PRACTICE, v.17, no.2, pp.267 - 279, 2009-02 |
| Satellite formation flying using along-track thrust Kumar, KD; Bang, Hyochoong; Tahk, Min-Jea, ACTA ASTRONAUTICA, v.61, no.7-8, pp.553 - 564, 2007-10 |
| Satellite orbit determination using GPS measurement Woo, H.W.; Tahk, Min-Jea; Jin, I.M.; Kim, J.C., Asia-Pacific Conference on Multilateral Corporation in Space Technology and Applications, 1996-05 |
| Scalar Adaptive Kalman Filtering for Stellar Inertial Attitude Determination Jung, Jae-Woo; Cho, Yun-Cheol; Bang, Hyo-Choong; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.3, no.2, pp.88 - 94, 2002-11 |
| Scalar Adaptive Kalman Filtering for Stellar Inertial Attitude Determination Jung, Jae-Woo; Cho, Yun-Cheol; Bang, Hyochoong; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.3, no.2, pp.88 - 94, 2002-11 |
| Sensitivity Analysis on Weight and Trajectory Optimization Results for Multistage Guided Missile Hong, Seong-Min; Seo, Min-Guk; Lee, Changhun; Tahk, Min-Jea; Shim, Sang-Wook, IFAC-PapersOnLine, pp.23 - 27, Elsevier B.V., 2016-08 |
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