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Prof. Chang-Hun Lee

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International Journal (SCI/SCIE)

 (*Corresponding Author)
  1. M. G. Seo, C. H. Lee*, and T. H. Kim, ¡°Trajectory Shaping Guidance Law using Constraint-Combining Multiplier,¡± Accepted for Publication in Proceedings for the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020.

  2. K. R. Song, T. H. Kim, C. H. Lee*, and M. J. Tahk, ¡°A New Guidance Algorithm against High-Speed Maneuvering Target,¡± Accepted for Publication in International Journal of Aeronautical and Space Sciences, 2020.

  3. H. S. Chi, Y. I. Lee, C. H. Lee, and H. L. Choi*, ¡°A Practical Optimal Guidance Scheme under Impact Angle and Terminal Acceleration Constraints,¡± Accepted for Publication in International Journal of Aeronautical and Space Sciences, 2020.

  4. C. Li, J. Wang, S. He*, and C. H. Lee, ¡°Collision-Geometry-Based Generalized Optimal Impact Angle Guidance for Various Missile and Target Motions,¡± Aerospace Science and Technology, Vol. 106, 2020.

  5. Y. C. Kim, C. H. Lee, T. H. Kim, and M. J. Tahk*, ¡°A New Cooperative Homing Guidance for Anti-ship Missiles for Survivability Enhancement,¡± Accepted for Publication in International Journal of Aeronautical and Space Sciences, 2020.

  6. D. Y. Lee, M. J. Tahk*, and C. H. Lee, ¡°Optimal Intermittent Maneuver of Homing Missiles for Target Observability Improvement,¡± Accepted for Publication in International Journal of Aeronautical and Space Sciences, 2020.

  7. N. Cho*, Y. Kim, and C. H. Lee, ¡°Schwarz Inequality Method for Weighted Minimum Effort Terminal Control of Multi-Dimensional Systems,¡± Journal of Guidance, Control, and Dynamics, Vol. 43, No. 10, pp. 1893-1903, 2020.

  8. S. He, C. H. Lee*, H. S. Shin, and A. Tsourdos, ¡°Optimal Three-Dimensional Impact Time Guidance with Seeker¡¯s Field-of-View Constraint,¡± Accepted for Publication in Chinese Journal of Aeronautics, 2020.

  9. K. Li, J. Wang, C. H. Lee, R. Zhou, and S. Zhao*, ¡°Distributed Cooperative Guidance for Multi-Vehicle Simultaneous Arrival without Numerical Singularities,¡± Journal of Guidance, Control, and Dynamics, Vol. 43, No. 7, pp. 1365-1373, 2020.

  10. C. H. Lee*, S. He, and J. H. Hong, ¡°Investigation on Physical Meaning of Three-Loop Autopilot,¡± International Journal of Control Automation and Systems, Vol. 18, pp. 2709-2720, 2020.

  11. J. H. Hong and C. H. Lee*, ¡°Nonlinear Autopilot Design for Endo- and Exo-Atmospheric Interceptor with Thrust-Vector-Control,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 56, No. 1, pp. 796-810, 2020.

  12. S. He, H. S. Shin*, A. Tsourdos, and C. H. Lee, ¡°Energy-Optimal Waypoint-Following Guidance Considering Autopilot Dynamic,¡± Accepted for publication in IEEE Transactions on Aerospace and Electronic Systems, Vol. 56, No. 4, pp. 2701-2717, 2020.

  13. S. M. Hong, M. J. Tahk*, and C. H. Lee, ¡°Stage Optimization of Anti-air Missiles using Practical Guidance Laws,¡± Accepted for publication in International Journal of Aeronautical and Space Sciences, Vol. 21, No. 2, pp. 394-403, 2020.

  14. Y. S. Jung, J. I. Lee, C. H. Lee, and M. J. Tahk*, ¡°A New Collision Control Guidance Law based on Speed Control for Kill Vehicles,¡± International Journal of Aeronautical and Space Sciences, Vol. 20, No. 3, 2019, pp. 792-805.

  15. C. H. Lee* and M. Y. Ryoo, ¡°Practical Generalized Optimal Guidance Law with Impact Angle Constraint,¡± Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering, Vol. 233, No. 10, 2019, pp. 3790-3809.

  16. S. He, C. H. Lee*, H. S. Shin, and A. Tsourdos, ¡°Minimum-Effort Waypoint-Following Guidance,¡± Journal of Guidance, Control, and Dynamics, Vol. 42, No. 7, 2019, pp. 1551-1561.

  17. J. H. Hong, S. S. Park, C. H. Lee, and C. K. Ryoo*, ¡°Study on Parasite Effect with Strapdown Seeker in Consideration of Time Delay,¡± Journal of Guidance, Control, and Dynamics, Vol. 42, No. 6, 2019, pp. 1383-1392.

  18. S. He and C. H. Lee*, ¡°Optimal Impact Angle Guidance for Exoatmospheric Interception Utilizing Gravitational Effect,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 55, No. 3, 2019, pp. 1382-1392.

  19. J. An, C. H. Lee, and M. J. Tahk*, ¡°A Collision Geometry-Based Guidance Law for Course-Correction-Projectile,¡± International Journal of Aeronautical and Space Sciences, Vol. 20, No. 2, pp. 442-458.

  20. S. He and C. H. Lee*, ¡°Optimal Proportional-Integral Guidance with Reduced Sensitivity to Target Maneuvers,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 54, No. 5, 2018, pp. 2568-2579.

  21. C. H. Lee* and M. G. Seo, ¡°New Insights into Guidance Laws with Terminal Angle Constraints,¡± Journal of Guidance, Control, and Dynamics, Vol. 41, No. 8, 2018, pp. 1832-1837.

  22. C. H. Lee, H. S. Shin*, A. Tsourdos, and Z. Skaf, ¡°A New Application of Data Analysis using Aircraft Fault Record Data,¡± Journal of Aerospace Information Systems, Vol. 15, No. 5, 2018, pp. 297-306.

  23. S. He and C. H. Lee*, ¡°Optimality of Error Dynamics in Missile Guidance Problems,¡± Journal of Guidance, Control, and Dynamics, Vol. 41, No. 7, 2018, pp. 1624-1633.

  24. S. He and C. H. Lee*, ¡°Gravity Turn-Assisted Optimal Guidance Law,¡± Journal of Guidance, Control, and Dynamics, Vol. 41, No. 1, 2018, pp. 171-183.

  25. M. J. Tahk*, S. W. Shim, S. M. Hong, C. H. Lee, and H. L. Choi, ¡°Impact Time Control Based on Time-to-Go Prediction for Sea-Skimming Anti-Ship Missiles,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 54, No. 4, 2018, pp. 2043-2052.

  26. C. H. Lee, H. S. Shin*, J. I. Lee, and M. J. Tahk, ¡°Zero-Effort-Miss Shaping Guidance Laws,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 54, No. 2, 2018, pp. 693-705.

  27. M. G. Seo*, C. H. Lee, and M. J. Tahk, ¡°New Design Methodology for Impact Angle Control Guidance for Various Missile and Target Motions,¡± IEEE Transactions on Control System Technology, Vol. 26, No. 6, 2018, pp. 2190-2197.

  28. C. H. Lee, B. E. Jun, J. I. Lee*, ¡°Connections between Linear and Nonlinear Missile Autopilots via Three Loop Topology,¡± Journal of Guidance, Control, and Dynamics, Vol. 39, No. 6, 2016, pp. 1426-1432.

  29. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Effects of Time-to-Go Errors on Performance of Optimal Guidance Laws,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 51, No. 1, 2015, pp. 3270-3281.

  30. M. Y. Ryu, C. H. Lee, and M. J. Tahk*, ¡°Command Shaping Guidance Law for High Speed Incoming Target,¡± Journal of Guidance, Control, and Dynamics, Vol. 38, No. 10, 2015, pp. 2025-2033.

  31. M. Y. Ryu, C. H. Lee, and M. J. Tahk*, ¡°New Trajectory Shaping Guidance Law for Anti-Tank Guided Missiles,¡± Proceedings for the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering, Vol. 229, No. 7, 2015, pp. 1360-1368.

  32. C. H. Lee*, J. I. Lee, and M. J. Tahk, ¡°Sinusoidal Weighted Optimal Guidance Laws,¡± Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering, Vol. 229, No. 3, 2015, pp. 534-542.

  33. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Biased PNG for Target Observability Enhancement against Nonmaneuvering Targets,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 51, No. 1, 2015, pp. 2-17.

  34. D. W. Yoo, C. H. Lee, M. J. Tahk*, and H. L. Choi, ¡°Optimal Resource Management Algorithm for UAV Missions in Hostile Territories,¡± Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering, Vol. 228, No. 12, 2014, pp. 2157-2167.

  35. C. H. Lee*, T. H, Kim, and M. J. Tahk, ¡°Agile Missile Autopilot Design using Nonlinear Backstepping Control with Time-Delay Adaptation,¡± Transactions of The Japan Society for Aeronautical and Space Sciences, Vol. 57, No. 1, 2014, pp. 9-20.

  36. J. I. Lee*, I. S. Jeon, and C. H. Lee, ¡°Command Shaping Guidance Law Based on Gaussian Weighting Function,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 50, No. 1, 2014, pp. 772-777.

  37. T. H. Kim*, C. H. Lee, M. J. Tahk, and I. S. Jeon, ¡°Augmented Polynomial Guidance with Impact Time and Angle Constraints,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 49, No. 4, 2013, pp. 2806-2817.

  38. T. H, Kim*, C. H. Lee, M. J. Tahk, and I. S. Jeon, ¡°Biased PNG Law for Impact-Time-Control,¡± Transactions of The Japan Society for Aeronautical and Space Sciences, Vol. 56, No. 4, 2013, pp. 205-214.

  39. C. H. Lee*, M. J. Tahk, and J. I. Lee, ¡°Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Constraint,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 49, No. 2, 2013, pp. 1317-1322.

  40. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Interception Angle Control Guidance using Proportional Navigation with Error Feedback,¡± Journal of Guidance, Control, and Dynamics, Vol. 36, No. 5, 2013, pp. 1556-1561.

  41. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Design of Impact Angle Control Guidance Laws via High-performance Sliding Mode Control,¡± Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering, Vol. 227, No. 2, Feb. 2013, pp. 235-253.

  42. T. H. Kim*, C. H. Lee, and M. J. Tahk, ¡°Time-to-go Polynomial Guidance with Trajectory Modulation for Observability Enhancement,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 49, No. 1, Jan. 2013, pp. 55-73.

  43. C. H. Lee*, T. H. Kim, M. J. Tahk, and I. H. Whang, ¡°Polynomial Guidance Laws Considering Terminal Impact Angle and Acceleration Constraints,¡± IEEE Transactions on Aerospace and Electronic Systems, Vol. 49, No. 1, Jan. 2013, pp. 74-92.

International Journal (Non-SCI/SCIE)

 (*Corresponding Author)
  1. C. H. Lee*, ¡°Linear Quadratic Optimal Guidance with Arbitrary Weighting Functions,¡± Journal of the Korea Society for Industrial and Applied Mathematics, Vol. 19, No. 3, 2015, pp. 365-386.

  2. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Augmented Time-to-go Polynomial Guidance Law for High Speed Target,¡± International Journal of Green Engineering and Management, Vol. 1, No. 1, 2012, pp. 65-76.

  3. S. M. Ryu*, D. W. Won, C. H. Lee, and M. J. Tahk, ¡°Missile Autopilot Design for Agile Turn Control during Boost-Phase,¡± International Journal of Aeronautical and Space Sciences, Vol. 12, No. 4, Dec. 2011, pp. 365-370.

  4. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Missile Autopilot Design for Agile Turn Using Time Delay Control with Nonlinear Observer,¡± International Journal of Aeronautical and Space Sciences, Vol. 12, No. 3, Sep. 2011, pp. 266-273.

  5. C. H. Lee* and M. J. Tahk, ¡°Unmanned Aerial Vehicle Recovery Using a Simultaneous Localization and Mapping Algorithm without the aid of Global Positioning System,¡± International Journal of Aeronautical and Space and Sciences, Vol. 11, No. 2, June 2010, pp. 98-109.

International Conference

 (*Corresponding Author)
  1. B. Kim, C. H. Lee*, M. J. Tahk, and S. He, ¡°A New Biased Proportional Navigation Guidance for Decelerating Targets,¡± 2020 International Conference on Guidance, Navigation, and Control (ICGNC 2020), Tanjin, China, 2020.

  2. Y. W. Kim, D. Y. Lee, M. J. Tahk, and C. H. Lee*, ¡°A New Path Planning Algorithm for Forced Landing of UAVs in Emergency Using Velocity Prediction Method,¡± 28th Mediterranean Conference on Control and Automation (MED), Saint-Raphael, France, 2020.

  3. D. Y. Lee, M. J. Tahk*, C. H. Lee, and Y. W. Kim, ¡°Singularity-Free Analytic Solution of Ballistic Trajectory with Quadratic Drag,¡± 28th Mediterranean Conference on Control and Automation (MED), Saint-Raphael, France, 2020.

  4. C. H. Lee* and M. J. Tahk, ¡°Autopilot Design for Unmanned Combat Aerial Vehicles (UCAVs) via Learning-based Approach,¡± 2019 IEEE Symposium Series on Computational Intelligence, 2019.

  5. Y. W. Kim, S. D. Lee, C. H. Lee*, H. S. Shin, and A. Tsourdos, ¡°A Nonlinear Attitude Controller for Drones with CMG (Control Momentum Gyro),¡± 2019 International Workshop on Research, Education and Development on Unmanned Aerial Systems, 2019.

  6. A. Tsourdos, I. A. D. Permana, D. H. Budiarti, H. S. Shin, and C. H. Lee, ¡°Developing Flight Control Policy Using Deep Deterministic Policy Gradient,¡± 2019 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology (ICARES), Indonesia, 2019.

  7. D. N. Vidal, C. H. Lee*, and A. Tsourdos, ¡°Sense and Avoid Using Hybrid Convolutional and Recurrent Neural Networks,¡± 21st IFAC Symposium on Automatic Control in Aerospace (ACA), 2019.

  8. H. Roh, Y. J. Oh, and M. J. Tahk*, and C. H. Lee, ¡°Fast Trajectory Optimization Using Sequential Convex Method for Guided Missiles,¡± 5th CEAS Conference on Guidance Navigation and Control, 2019.

  9. S. J. Bae, H. S. Shin*, C. H. Lee, and A. Tsourdos, ¡°A New Multiple Flights Routing and Scheduling Algorithm in Terminal Manoeuvering Area,¡± 2018 IEEE/AIAA 37th Digital Avionics Systems Conference (DASC), 2018.

  10. C. H. Lee* and A. Tsourdos, ¡°Cooperative Control for Multiple Interceptors to Maximize Collateral Damage,¡± IFAC Workshop on Networked & Autonomous Air & Space Systems (NAASS 2018), June, Santa Fe, USA, 2018.

  11. M. S. Fabregas, C. H. Lee*, and A. Tsourdos, ¡°A Group-Based Navigation Algorithm for Multiple Anti-Ship Missile Systems,¡± 2018 European Control Conference, June, Cyprus, 2018.

  12. C. H. Lee*, H. S. Shin, A. Tsourdos, and S. Zakwan, ¡°Data Analytics Development of FDR (Flight Data Recorder) Data for Airline Maintenance Operations,¡± 2017 IEEE International Conference on Multisensor Fusion and Integration for Intelligent Systems (MFI 2017), Nov. 16-18, 2017, Daegu, Korea.

  13. C. H. Lee*, H. S. Shin, A. Tsourdos, Z. Skaf, ¡°Data Mining of FDR(flight data recorder) Data for Enhancing Airline Maintenance Operations,¡± The 3rd International Conference on Intelligent Signal Processing (ISP 2017), London, UK, 2017.

  14. M. Zarudzki, H. S. Shin*, and C. H. Lee, ¡°An Image Based Visual Servoing Approach for Multi-Target Tracking using an Quad-tilt Rotor UAV,¡± 2017 International Conference on Unmanned Aircraft Systems (ICUAS), Miami, USA, 2017.

  15. C. H. Lee*, H. S. Shin, A. Tsourdos, and J. I. Lee, ¡°A New Command Shaping Guidance Law using Lagrange Multiplier,¡± 20th International Federation of Automatic Control (IFAC) World Congress, Toulouse, France, 2017.

  16. C. H. Lee*, B. E. Jun, H. S. Shin, and A. Tsourdos, ¡°Nonlinear Acceleration Controller for Exo-Atmospheric and Endo-Atmospheric Interceptors with TVC,¡± 25th Mediterranean Conference on Control and Automation, Malta, 2017.

  17. S. M. Hong*, M. G. Seo, S. W. Shim, M. J. Tahk, and C. H. Lee, ¡°Sensitivity Analysis on Weight and Trajectory Optimization Results for Multistage Guided Missile,¡± 20th International Federation of Automatic Control (IFAC) Symposium on Automatic Control in Aerospace, Sherbrooke, Canada, 2016.

  18. M. G. Seo*, C. H. Lee, M. J. Tahk, J. I. Lee, and B. E. Jun, ¡°Control Input Blending Logic with Aerodynamic Control and Reaction Jet Control,¡± 29th Congress of the International Council of the Aeronautical Sciences, St. Petersburg, Russia, 2014.

  19. B. E. Jun and C. H. Lee*, ¡°Integrated Pitch/Yaw Acceleration Controller for Projectile with Rotating Canards using Linear Quadratic Control Methodology,¡± IEEE Multi-Conference on Systems and Control, Nice, France, 2014.

  20. H. J. Lee, C. H. Lee*, and B. E. Jun, ¡°Autopilot Design for Dual-Spin Projectile based on PI and Feedback Linearization Control,¡± IEEE Multi-Conference on Systems and Control, Nice, France, 2014.

  21. C. H. Lee* and B. E. Jun, ¡°Guidance Algorithm for Projectile with Rotating Canards via Predictor-Corrector Approach,¡± Accepted for presentation on IEEE Multi-Conference on Systems and Control, Nice, France, 2014.

  22. C. H. Lee*, Y. W. Lee, B. E. Jun, and M. J. Tahk, ¡°Design of Missile Autopilot using PI and Approximate Feedback Linearization Control with Time-Delay Adaptation Scheme,¡± 2014 European Control Conference (ECC) June 24-27, Strasbourg, France, 2014, pp. 2762-2767.

  23. C. H. Lee*, B. E. Jun, J. I. Lee, and M. J. Tahk, ¡°Nonlinear Missile Autopilot Design via Three Loop Topology and Time-Delay Adaptation Scheme,¡± International Conference on Control, Automation and Systems 2013, KCC, Gwangju, Korea, Oct. 2013.

  24. C. H. Lee*, D. W. Yoo, G. H. Moon, and M. J. Tahk, ¡°Resource Management Algorithm for Suppression of Enemy Air Defense (SEAD) Mission,¡± 2012 Asia-Pacific International Symposium on Aerospace Technology, Jeju, Korea, Nov. 2012.

  25. G. H. Moon*, C. H. Lee, D. W. Yoo, and M. J. Tahk, ¡°Distributed Cooperative Control Algorithm for SEAD Mission of Heterogeneous UAVs,¡± 2012 Asia-Pacific International Symposium on Aerospace Technology, Jeju, Korea, Nov. 2012.

  26. M. G. Seo*, C. H. Lee, M. J. Tahk, J. I. Lee, and B. E. Jun, ¡°Design of Missile Acceleration Autopilot Using Approximate System and Backstepping Control,¡± 2012 Asia-Pacific International Symposium on Aerospace Technology, Jeju, Korea, Nov. 2012.

  27. J. I. Lee*, I. S. Jeon, and C. H. Lee, ¡°A New Guidance Law Based on Gaussian Weighting Function,¡± 2012 Asia-Pacific International Symposium on Aerospace Technology, Jeju, Korea, Nov. 2012.

  28. M. G. Seo*, C. H. Lee, and M. J. Tahk, ¡°Comparison Study on Adaptive Law Structures for Nonlinear Missile Autopilot,¡± The Japan Society for Aeronautical and Space Sciences, Fukuoka, Japan, Nov. 2012.

  29. G. H. Moon*, C. H. Lee, D. W. Yoo, and M. J. Tahk, ¡°Consensus Based Bundle Algorithm for Air to Air Weapon Assignment,¡± The Japan Society for Aeronautical and Space Science, Fukuoka, Japan, Nov. 2012.

  30. C. H. Lee*, M. J. Tahk, and B. E. Jun, ¡°Autopilot Design for an Agile Missile Using L1 Adaptive Backstepping Control,¡± 28th International Congress of the Aeronautical Sciences, Brisbane, Australia, Sep. 2012.

  31. C. H. Lee*, K. S. Kim, and M. J. Tahk, ¡°Longitudinal Autopilot Design for Agile Turn Using Mixed H2/H-infinity Control,¡± International Conference on Control, Automation, and Systems 2011, KINTEX, Korea, Oct. 2011.

  32. T. H. Kim*, C. H. Lee, and M. J. Tahk, ¡°Time-to-go Polynomial Guidance Laws with Terminal Impact Angle/Acceleration Constraints,¡± 18th IFAC World Congress, Milano, Italy, Aug. 2011.

  33. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Augmented Time-to-go Polynomial Guidance Law for High Speed Target,¡± YUST International Symposium 2011, YUST, China, June. 2011.

  34. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Design of Guidance Law for Passive Homing Missile Using Sliding Mode Control,¡± International Conference on Control, Automation, and Systems 2010, KINTEX, Korea, Oct. 2010.

  35. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Observability Analysis of Advanced Guidance Laws with Bearing-Only Measurement,¡± 18th IFAC Symposium on Automatic Control in Aerospace, Nara, Japan, Sep. 2010.

  36. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Target Observability Enhanced Impact Angle Control Guidance Law Using Composite Non-linear Feedback Control,¡± 2010 Asia-Pacific International Symposium on Aerospace Technology, Xian, China, Sep. 2010.

  37. K. U. Kim, S. H. Kang, H. J. Kim*, C. H. Lee, and M. J. Tahk, ¡°Realtime Agile-Turn Guidance and Control for an Air-to-Air Missile,¡± AIAA Guidance, Navigation, and Control Conference, Toronto, Ontario, Canada, Aug. 2010.

  38. S. M. Ryu*, D. Y. Won, C. H. Lee, and M. J. Tahk, ¡°High Angle of Attack Missile Autopilot Design by Pole Placement Approach,¡± The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, Harbin, China, June. 2010.

  39. C. H. Lee*, T. H. Kim, and M. J. Tahk, ¡°Real Time Path-planning Algorithm and Guidance Logic for the Glider Bomb,¡± ICCAS-SICE09, Fukuoka, Japan, Aug. 2009.

Domestic Journal

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Domestic Conference

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  5. ±èº¸¼®, Á¤ÅÂÈ£, ÀÌâÈÆ, ¡°Ç×·Î ÃßÁ¾ À¯µµ ¹ýÄ¢À» ÀÌ¿ëÇÑ ´Ù¼ö ¹«ÀÎÇ×°ø±â ¸ñÇ¥¹° ÃßÀû ±â¹ý,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2020 Ãß°èÇмú´ëȸ, Á¦ÁÖµµ, 2020.

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  7. À±´ÙÀÎ, ±è¿µ¿ø, ÀÌâÈÆ, ¡°°³Àοë Ç×°ø±âÀÇ ºñ¼±Çü ÀÚ¼¼°¢ Á¦¾î±â ¼³°è,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2020³âµµ Ãá°èÇмú´ëȸ, 2020.

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  9. ±èº¸¼®, ±è¿µ¿ø, ÀÌâÈÆ, ¡°Ãæµ¹ À¯µµ±âÇϸ¦ ±â¹ÝÀ¸·Î ÇÑ ÅëÇÕµÈ Àü¸é/Èĸé Ãæµ¹ À¯µµ ±â¹ý,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2020³âµµ Ãá°èÇмú´ëȸ, 2020.

  10. ÀÌâÈÆ, ¾ÈÀç¸í, ±èÁ¾ÇÑ, ¡°¹ß»çü Àç»ç¿ëÀ» À§ÇÑ ÀçÁøÀÔ ¹× Âø·ú ¿¬±¸,¡± Çѱ¹ÃßÁø°øÇÐȸ 2019³âµµ Ãß°èÇмú´ëȸ, 2019.

  11. È«¼º¹Î, ÀÌâÈÆ, Ź¹ÎÁ¦, ¡°´ë°ø À¯µµÅºÀÇ °¡»óÇ¥Àû À§Ä¡°¡ ÃÖÀû ´Ü Áß·®¿¡ ¹ÌÄ¡´Â ¿µÇ⠺м®,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2019³âµµ Ãß°èÇмú´ëȸ, 2019.

  12. ±è¿µ¿ø, ÀÌ»óµ·, ÀÌâÈÆ, ÃÖÇѸ², À¯¿ª, ¡°ÀçÁøÀÔ ºñÇàü Ư¼º¿¡ µû¸¥ ÀçÁøÀÔ ´Ü°è ºñÇà ¿µ¿ª ºÐ¼®,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2019³âµµ Ãß°èÇмú´ëȸ, 2019.

  13. ÀÌ»óµ·, ±è¿µ¿ø, ÀÌâÈÆ, ÃÖÇѸ², À¯Çõ, ¡°ÀçÁøÀÔ ºñÇàüÀÇ 3-·çÇÁ ±â¹Ý ºñ¼±Çü ¹ÞÀ½°¢ Á¦¾î±â ¼³°è,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2019³âµµ Ãß°èÇмú´ëȸ, 2019.

  14. ÀÌ»óµ·, È«¼º¹Î, ÀÌâÈÆ, ¡°Àç»ç¿ë ¹ß»çüÀÇ ±ËÀû ÃÖÀûÈ­¿¡ °üÇÑ ÀÎÀÚ ¿¬±¸,¡± Á¦18ȸ ¿ìÁֹ߻çü±â¼ú ½ÉÆ÷Áö¾ö, 2019.

  15. ÀÌâÈÆ, ÀÌ»óµ·, ¡°Physical Meanings of Optimal Control in Guidance Applications,¡± Çѱ¹»ê¾÷ÀÀ¿ë¼öÇÐȸ 2019³âµµ Ãá°èÇмú´ëȸ, 2019.

  16. ÀÌâÈÆ, ÀÌ»óµ·, ±èÅÂÈÆ, ¼Û°æ·Ï, ¡°Ç¥Àû °¨¼ÓÀ» °í·ÁÇÑ ÆíÇâ ºñ·ÊÇ×¹ýÀ¯µµ¹ýÄ¢ ¿¬±¸,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2019³âµµ Ãá°èÇмú´ëȸ, 2019.

  17. ¾ÈÁö¿¬, À̼®¿ì, ¼Û¹Î¼·, ÀÌÇÑÁø, Á¤¸í¼÷, ÀÌâÈÆ, ¡°ÅºµµÁ¶Á¾½Å°üÀÇ ±â´É °ËÁõÀ» À§ÇÑ ½ÃÇè ȯ°æ ±¸Ãà,¡± Çѱ¹±º»ç°úÇбâ¼úÇÐȸ 2018³âµµ Ãß°èÇмú´ëȸ, 2018.

  18. ÀÌâÈÆ, ³ª¿ø»ó, Á¤º¸¿µ, ¡°Á¤º¸·® ÃÖ´ëÈ­ À¯µµ±â¹ý ºñ±³ ºÐ¼®,¡± 2018³âµµ Á¤º¸ ¹× Á¦¾î Çмú´ëȸ, 2018.

  19. ÀÌÇÑÁø, ±Ç±âº¹, ÀÌâÈÆ, ¾ÈÁö¿¬, ¡°ÅºµµÁ¶Á¾½Å°üÀÇ Ç×¹ý ¹× À¯µµ ±â¹ý ¿¬±¸,¡± Çѱ¹±º»ç°úÇбâ¼úÇÐȸ 2015³âµµ Ãá°èÇмú´ëȸ, 2015.

  20. ÀÌÁøÀÍ, ÀÌâÈÆ, ¼Û°æ·Ï, ¡°ÅºµÎ À§·Â Áõ´ë¸¦ À§ÇÑ Á¾¸» ±âµ¿ ¿¬±¸,¡± Çѱ¹±º»ç°úÇбâ¼úÇÐȸ 2015³âµµ Ãß°èÇмú´ëȸ, 2015.

  21. ÀÌâÈÆ, ±èÅÂÈÆ, Àüº´À», ¡°¶ó±×¶ûÁö ½Â¼ö¸¦ ÀÌ¿ëÇÑ ±ËÀû ¼ºÇü À¯µµ ±â¹ý,¡± Çѱ¹±º»ç°úÇбâ¼úÇÐȸ 2015³âµµ Ãá°èÇмú´ëȸ, 2015.

  22. ±èÅÂÈÆ, ÀÌâÈÆ, Àüº´À», ¡°ÅºµµÅº ¹æ¾î¸¦ À§ÇÑ ¿¹»ó¸íÁßÁ¡ ¿¹Ãø±â¹ý,¡± Çѱ¹±º»ç°úÇбâ¼úÇÐȸ 2015³âµµ Ãá°èÇмú´ëȸ, 2015.

  23. ÀÌâÈÆ, ±èÅÂÈÆ, Àüº´À», ¡°¼ø°£ ÀÚÀ¯³«ÇÏ ±ËÀûÀ» ÀÌ¿ëÇÑ ¿ä°ÝüÀÇ Áß±âÀ¯µµ ±â¹ý,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2015³âµµ Ãá°èÇмú´ëȸ, 2015.

  24. ÀÌâÈÆ, Àüº´À», ÀÌÁøÀÍ, ¡°À¯µµÅº 3-·çÇÁ ¼±Çü Á¦¾î±â¿Í ºñ¼±Çü Á¦¾î±âÀÇ »ó»ç¼º ºÐ¼®,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2015³âµµ Ãá°èÇмú´ëȸ, 2015.

  25. ÀÌâÈÆ, Àüº´À», ±Ç±âº¹, ¡°ÇÊÅÍ ±¸Á¶¿¡ µû¸¥ źµµ¼öÁ¤½Å°ü ·Ñ°¢ ÃßÁ¤±â ¼º´ÉºÐ¼®,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2015³âµµ Ãá°èÇмú´ëȸ, 2015.

  26. ¾ÈÁö¿¬, ÀÌâÈÆ, ÀÌÇÑÁø, ¡°ÅºµµÁ¶Á¾½Å°ü ¸ðµ¨¸µ,¡± Á¦17ȸ À¯µµ¹«±âÇмú´ëȸ, 2014.

  27. ÀÌâÈÆ, ±èÅÂÈÆ, Àüº´À», ¡°DACSÇü Á÷°Ý¿ä°ÝºñÇàüÀÇ ºñ¼±Çü °¡¼Óµµ Á¶Á¾·çÇÁ ¼³°è,¡± Çѱ¹ÃßÁø°øÇÐȸ 2014³âµµ Ãß°èÇмú´ëȸ, 2014.

  28. ±èÅÂÈÆ, ÀÌâÈÆ, Àüº´À», ¡°TVC±â¹Ý °íüÃßÁø·ÎÄÏÀÇ °¡¼Óµµ Á¦¾î·çÇÁ ¼³°è,¡± Çѱ¹ÃßÁø°øÇÐȸ 2014³âµµ Ãß°èÇмú´ëȸ, 2014.

  29. ÀÌÁøÀÍ, ÀÌâÈÆ, ¡°Á߷¿¡ ÀÇÇÑ È£¹Ö ±ËÀûÀ» °í·ÁÇÑ È¿°úÀûÀÎ Á¾¸»À¯µµ ¼±µµ °¢ º¸Á¤ ¹æ¹ý,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2014³âµµ Ãß°èÇмú´ëȸ, 2014.

  30. ÀÌâÈÆ, ±èÅÂÈÆ, Àüº´À», ¡°3-·çÇÁ ±â¹Ý ºñ¼±Çü À¯µµÅº Á¶Á¾·çÇÁÀÇ ÀÀ´äƯ¼º ºÐ¼®,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2014³âµµ Ãß°èÇмú´ëȸ, 2014.

  31. À¯µ¿¿Ï, ÀÌâÈÆ, Ź¹ÎÁ¦, ÃÖÇѸ², ¡°ÀüÀå¿¡¼­ÀÇ ¹«ÀÎ Ç×°ø±â ÃÖÀû ¹èÄ¡ ¾Ë°í¸®Áò,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2014³âµµ Ãá°èÇмú´ëȸ, 2014.

  32. ÀÌâÈÆ, Àüº´À», ¡°Á¦¾î±¸Á¶¿¡ µû¸¥ źµµ¼öÁ¤½Å°ü Á¶Á¾¼º´É ºÐ¼®,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2014³âµµ Ãá°èÇмú´ëȸ, 2014.

  33. ÀÌÁøÀÍ, ¼Û°æ·Ï, ÀÌâÈÆ, ¡°ÀϽĿµ¿ªÀÇ ½ÅÈ£´ë ÀâÀ½ºñ ÃßÁ¤±â ¼³°è,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2013³âµµ Ãß°èÇмú´ëȸ, 2013.

  34. ÀÌâÈÆ, ±èÅÂÈÆ, ÀÌÁøÀÍ, Ź¹ÎÁ¦, ¡°ÀÜ¿©ºñÇà½Ã°£ °¡ÁßÇÔ¼ö¸¦ ÀÌ¿ëÇÑ ZEM ±â¹Ý È£¹ÖÀ¯µµ ¹ýÄ¢,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2013³âµµ Ãß°èÇмú´ëȸ, 2013.

  35. ¼­¹Î±¹, ÀÌâÈÆ, Ź¹ÎÁ¦, ¡°Ptolemy II¸¦ ÀÌ¿ëÇÑ À¯µµÅº ÀÚµ¿ Á¶Á¾ ½Ã¹Ä·¹ÀÌ¼Ç ¸ðµ¨ °³¹ß,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2013³âµµ Ãá°èÇмú´ëȸ, 2013.

  36. ÀÌâÈÆ, ÀÌÁøÀÍ, Ź¹ÎÁ¦, ¡°ÀϹÝÈ­ µÈ ÃÖÀû È£¹Ö À¯µµ¹ýÄ¢ ¿¬±¸,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2013³âµµ Ãá°èÇмú´ëȸ, 2013.

  37. ¼­¹Î±¹, ÀÌâÈÆ, Ź¹ÎÁ¦, ¡°½Ã°£ Áö¿¬ ÀûÀÀ ¹é½ºÅ×ÇÎ Á¦¾î¸¦ ÀÌ¿ëÇÑ À¯µµÅºÀÇ °¡¼Óµµ Á¦¾î±â ¼³°è,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2012³âµµ Ãá°èÇмú´ëȸ, 2012.

  38. ÀÌâÈÆ, ½ÅÈ¿»ó, Ź¹ÎÁ¦, ¡°SEAD ÀÓ¹«¸¦ À§ÇÑ ¹«ÀαâÀÇ ºÐ»êÇù¾÷Á¦¾î ¾Ë°í¸®Áò ¿¬±¸,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2011³âµµ Ãß°èÇмú´ëȸ, 2011.

  39. ÀÌâÈÆ, ±èÅÂÈÆ, Ź¹ÎÁ¦, ȲÀÍÈ£, ¡°Ç¥Àû °¡°üÃø¼º Çâ»óÀ» À§ÇÑ Biased PNG ¼³°è,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2010³âµµ Ãß°èÇмú´ëȸ, 2010.

  40. ÀÌâÈÆ, ±èÅÂÈÆ, Ź¹ÎÁ¦, ȲÀÍÈ£, ¡°½½¶óÀ̵ù ¸ðµå Á¦¾î ±â¹ýÀ» ÀÌ¿ëÇÑ ÀÚµ¿Á¶Á¾ÀåÄ¡ÀÇ ½Ã°£ Áö¿¬ÀÌ °í·Á µÈ À¯µµ ¹ýÄ¢ ¿¬±¸,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2010³âµµ Ãß°èÇмú´ëȸ, 2010.

  41. ·ù¼±¹Ì, ÀÌâÈÆ, Ź¹ÎÁ¦, ±èÇöÁø, Àüº´À», ÀÌÁøÀÍ, ¡°±â¹Î ȸÀü À¯µµÅºÀ» À§ÇÑ ½Ç½Ã°£ À¯µµ ¹ýÄ¢ ¿¬±¸,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2010³âµµ Ãß°èÇмú´ëȸ, 2010.

  42. ½É»ó¿í, ¿ø´ë¿¬, ÀÌâÈÆ, Ź¹ÎÁ¦, ¼º±âÁ¤, ±èÀÀÅÂ, ¡°Sub-Window ±â¹Ý HMM ÇÊÅ͸¦ ÀÌ¿ëÇÑ ´Ù¼ö Ç¥Àû ŽÁö ±â¹ý,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2010³âµµ Ãß°èÇмú´ëȸ, 2010.

  43. Á¤±Õ¸í, ¼ºÀç¹Î, ±èº´¼ö, ÀÌâÈÆ, Ź¹ÎÁ¦, ¡°À¯µµÆ÷źÀÇ ½Å°æȸ·Î¸Á ±â¹Ý ÀûÀÀÁ¦¾î±â ¼³°è ¿¬±¸,¡± Çѱ¹±º»ç°úÇбâ¼úÇÐȸ 2010 Á¾ÇÕÇмú´ëȸ, 2010.

  44. ¿ø´ë¿¬, ·ù¼±¹Ì, ÀÌâÈÆ, Ź¹ÎÁ¦, ¡°À¯µµÅºÀÇ ¹«°ÔÁ᫐ º¯È­¸¦ °í·ÁÇÑ ¼±ÇüÇà·ÄºÎµî½Ä(LMI)±â¹Ý °­°Ç Á¦¾î±â ¼³°è,¡± Á¦¾î·Îº¿½Ã½ºÅÛÇÐȸ 2010³âµµ Ãá°èÇмú´ëȸ, °­¿øµµ, 2010.

  45. ÀÌâÈÆ, ±èÅÂÈÆ, Ź¹ÎÁ¦, ¡°°ø´ë°ø À¯µµÅºÀÇ ±â¹ÎÇÑ È¸ÀüÀ» À§ÇÑ ºñ¼±Çü Á¦¾î±â ¼³°è,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2009³âµµ Ãß°èÇмú´ëȸ, 2009.

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  47. ÀÌâÈÆ, ±èÅÂÈÆ, ·ù¼±¹Ì, Ź¹ÎÁ¦, ¡°±ËÀû ÃÖÀûÈ­¸¦ ÅëÇÑ ±â¹ÎÇÑ À¯µµÅºÀÇ È¸Àü±âµ¿ ºÐ¼®,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2009³âµµ Ãá°èÇмú´ëȸ, 2009.

  48. ÀÌâÈÆ, Ź¹ÎÁ¦, ¡°SLAMÀ» ÀÌ¿ëÇÑ UAVÀÇ ÀÚµ¿ Ç×¹ý¿¡ °üÇÑ ¿¬±¸,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2009³âµµ Ãá°èÇмú´ëȸ, 2009.

  49. ±èÀ±È¯, ¹ÚÁ¤¿ì, ÀÌâÈÆ, Ź¹ÎÁ¦, ¡°´Ü°Å¸® °ø´ë°ø À¯µµÅºÀÇ 180µµ ȸÀü±âµ¿ Çؼ®À» À§ÇÑ Á¦¾îÀÔ·Â ÀÌ»êÈ­ ¹× ÃÖÀûÈ­ ±â¹ý,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2009³âµµ Ãá°èÇмú´ëȸ, 2009.

  50. ¹ÚºÀ±Õ, ÀÌâÈÆ, »ó´ë±Ô, ±èÅÂÈÆ, Ź¹ÎÁ¦, ¡°´Þ Âø·úÀ» À§ÇÑ ±ËÀûÃÖÀûÈ­ ¿¬±¸,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2008³âµµ Ãß°èÇмú´ëȸ, 2008.

  51. ÀÌâÈÆ, ±èÅÂÈÆ, Ź¹ÎÁ¦, ¡°±Û¶óÀÌ´õ ÆøźÀÇ ½Ç½Ã°£ °æ·Î °èȹ¿¡ °üÇÑ ¿¬±¸,¡± Çѱ¹Ç×°ø¿ìÁÖÇÐȸ 2008³âµµ Ãß°èÇмú´ëȸ, 2008.