Browse "Dept. of Aerospace Engineering(항공우주공학과)" by Author Tahk, Min-Jea
Showing results 353 to 412 of 485
| 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 |
| Sensor Alignment Calibration for Precision Attitude Determination of Spacecraft Lee, Il-Hyoung; Ryoo, Chang-Kyung; Bang, Hyochoong; Tahk, Min-Jea; Lee, Sang-Ryool, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.5, no.1, pp.83 - 93, 2004-05 |
| Sensor Alignment Calibration for Precision Attitude Determination of Spacecraft Lee, Il-Hyoung; Ryoo, Chang Kyung; Bang, Hyochoong; Tahk, Min-Jea; Lee, Sang-Ryool, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.5, no.1, pp.83 - 93, 2004-05 |
| Short-time stability of proportional navigation guidance loop Rew, DY; Tahk, Min-Jea; Cho, HJ, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.32, no.3, pp.1107 - 1115, 1996-07 |
| Singularity Avoidance Law for CMG using Virtual Actuator Lee, H; Lee, D; Bang, Hyochoong; Tahk, Min-Jea, 17th IFAC Symposium on Automatic Control in Aerospace, IFAC, 2007-06-25 |
| Singularity-Free Analytic Solution of Ballistic Trajectory with Quadratic Drag Lee, Dong-Yeon; Tahk, Min-Jea; Lee, Chang-Hun; KIM, Youngwon, 28th Mediterranean Conference on Control and Automation, MED 2020, pp.249 - 253, Institute of Electrical and Electronics Engineers Inc., 2020-09-17 |
| Sinusoidal function weighted optimal guidance laws Lee, Chang-Hun; Lee, Jin-Ik; Tahk, Min-Jea, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.229, no.3, pp.534 - 542, 2015-03 |
| SLUNG-LOAD TRAJECTORY CONTROL USING AN INPUT-SHAPING METHOD WITH MODEL-FOLLOWING CONTROL Lee, Byung-Yoon; Oh, Hyun-Shik; Tahk, Min-Jea; Lee, Hae-In, INTERNATIONAL JOURNAL OF ROBOTICS & AUTOMATION, v.37, no.1, pp.60 - 75, 2022 |
| Spacecraft attitude control using quaternion parameters Yoon, H.J.; Tahk, Min-Jea, Korea Automatic Control Conference, 1995-10 |
| Stability of homing guidance loop with missile dynamics = 미사일 다이내믹스를 고려한 호우밍 유도 루우프의 안정성 해석link Rew, Dong-Young; 류동영; et al, 한국과학기술원, 1996 |
| Stage Optimization of Anti-Air Missiles Considering Guidance Laws Hong, Seong-Min; Lee, Dong-Yeon; Tahk, Min-Jea, 21st International-Federation-of-Automatic-Control (IFAC) Symposium on Automatic Control in Aerospace (ACA), pp.227 - 231, ELSEVIER, 2019-08 |
| Stage Optimization of Anti-air Missiles Using Practical Guidance Laws Hong, Seong-Min; Tahk, Min-Jea; Lee, Chang-Hun, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.21, no.2, pp.394 - 403, 2020-06 |
| Stage optimization of multi-stage anti-air missile using co-evolutionary augmented Lagrangian method Hong, Seong-Min; Tahk, Min-Jea, 25th Mediterranean Conference on Control and Automation, MED 2017, pp.1257 - 1262, Institute of Electrical and Electronics Engineers Inc., 2017-07 |
| Station collocation design algorithm for multiple geostationary satellites operation Park, BK; Tahk, Min-Jea; Bang, Hyochoong; Choi, SB, JOURNAL OF SPACECRAFT AND ROCKETS, v.40, no.6, pp.889 - 893, 2003-11 |
| Stationkeeping of an airship Park, C.S.; Bang, Hyochoong; Tahk, Min-Jea, ICCAS 2001, 2001-10 |
| Stellar Adaptive Kalman Filtering for Stellar Inertial Attitude Determination Jung, JW; Cho, YC; Bang, Hyochoong; Tahk, Min-Jea, 16th JSASS Aircraft Symposium, pp.189 - 192, 2002-10 |
| Study on an auto-landing guidance for UAV with engine flame-out = 무인항공기 엔진 정지 시 자동착륙 유도에 대한 연구link Kim, Young-Sam; Tahk, Min-Jea; et al, 한국과학기술원, 2019 |
| Study on guidance laws for course-correction-projectile using trajectory error shaping = 궤적 오차 성형을 이용한 탄도수정탄 유도기법 연구link An, Ji-Yeon; Tahk, Min-Jea; et al, 한국과학기술원, 2019 |
| Study on Guidance Laws of Varying-Velocity Missiles = 속도 변화를 고려한 유도탄의 유도기법 연구link Seo, Min-Guk; 서민국; et al, 한국과학기술원, 2017 |
| Study on payload stabilization method with the slung-load transportation system using a quad-rotor Lee, Byung Yoon; Lee, Hae-In; Yoo, Dong Wan; Moon, Gun-Hee; Lee, Dong-Yeon; Kim, Yun Young; Tahk, Min-Jea, European Control Conference, ECC 2015, pp.2097 - 2102, Institute of Electrical and Electronics Engineers Inc., 2015-07 |
| Study on vertical landing of unmanned aerial vehicle using thrusters = 추력기를 이용한 무인기의 수직 착륙에 관한 연구link Han, Seungyeop; Tahk, Min-Jea; et al, 한국과학기술원, 2017 |
| Suboptimal Guidance Based on Pursuit and Impact Angle Control for Long-Range Air-to-Air Missiles Tahk, Min-Jea; Park, Jong-Chan; Rho, Heekun; Lee, Chang-Hun, 2023 14th International Conference on Mechanical and Aerospace Engineering, IEEE, Science and Engineering Institute, 2023-07-20 |
| Suboptimal guidance for passive homing missiles with angle-only-measurement Lee, H.I.; Lee, H.G.; Tahk, Min-Jea, 15th IFAC Symposium on Automatic Control in Aerospace, 2001-09 |
| Suboptimal guidance laws with terminal jerk constraint Lee, J.-I.; Min, B.-M.; Tahk, Min-Jea, International Conference on Control, Automation and Systems, ICCAS 2007, pp.1399 - 1403, 2007-10-17 |
| Suboptimal mid-course guidance algorithm for accelerating missiles Seo, Min-Guk; Tahk, Min-Jea, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.231, no.11, pp.2032 - 2047, 2017-09 |
| Suboptimal midcourse guidance law for interception of free-fall targets Song, E.J.; Tahk, Min-Jea, AIAA Conference on Guidance, Navigation, and Control, AIAA, 1999-08 |
| Survivability enhanced 3-D biased proportional navigation guidance laws Kim, YH; Ryoo, CK; Tahk, Min-Jea, JSASS 17th Aircraft Symposium, JSASS, 2003-10 |
| Synthesis and Investigation of the Neural Network Guidance based on Pursuit-evasion Games Choi, Han-Lim; Bang, Hyochoong; Tahk, Min-Jea; Lee, H.G., ICCAS 2001, ICCAS, 2001-10 |
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