Optimal guidance laws with terminal impact angle constraint CK Ryoo, H Cho, MJ Tahk Journal of Guidance, Control, and Dynamics 28 (4), 724-732, 2005 | 630 | 2005 |
Time-to-go weighted optimal guidance with impact angle constraints CK Ryoo, H Cho, MJ Tahk IEEE Transactions on control systems technology 14 (3), 483-492, 2006 | 498 | 2006 |
Fault tolerant control for satellites with four reaction wheels J Jin, S Ko, CK Ryoo Control Engineering Practice 16 (10), 1250-1258, 2008 | 238 | 2008 |
Recursive time-to-go estimation for homing guidance missiles MJ Tahk, CK Ryoo, H Cho IEEE Transactions on Aerospace and electronic Systems 38 (1), 13-24, 2002 | 148 | 2002 |
Closed-form solutions of optimal guidance with terminal impact angle constraint CK Ryoo, H Cho, MJ Tahk Proceedings of 2003 IEEE Conference on Control Applications, 2003. CCA 2003 …, 2003 | 133 | 2003 |
Closed-form optimal guidance law for missiles of time-varying velocity H Cho, CK Ryoo, MJ Tahk Journal of Guidance, Control, and Dynamics 19 (5), 1017-1022, 1996 | 108 | 1996 |
Line-of-sight guidance laws for formation flight MJ Tahk, CS Park, CK Ryoo Journal of Guidance, Control, and Dynamics 28 (4), 708-716, 2005 | 89 | 2005 |
Optimal guidance with constraints on impact angle and terminal acceleration YI Lee, CK Ryoo, E Kim AIAA guidance, navigation, and control conference and exhibit, 5795, 2003 | 86 | 2003 |
Optimal impact angle control guidance law based on linearization about collision triangle H Cho, CK Ryoo, A Tsourdos, B White Journal of Guidance, Control, and Dynamics 37 (3), 958-964, 2014 | 82 | 2014 |
A tight path following algorithm of an UAS based on PID control I Rhee, S Park, CK Ryoo Proceedings of SICE annual conference 2010, 1270-1273, 2010 | 79 | 2010 |
Implementation of optimal guidance laws using predicted missile velocity profiles H Cho, CK Ryoo, MJ Tahk Journal of Guidance, Control, and Dynamics 22 (4), 579-588, 1999 | 66 | 1999 |
Guidance algorithms for tactical missiles with strapdown seeker SA Jang, CK Ryoo, K Choi, MJ Tahk 2008 SICE Annual Conference, 2616-2619, 2008 | 57 | 2008 |
Energy optimal waypoint guidance synthesis for antiship missiles CK Ryoo, HS Shin, MJ Tahk IEEE Transactions on Aerospace and Electronic Systems 46 (1), 80-95, 2010 | 49 | 2010 |
Guidance and control for missiles with a strapdown seeker D Kim, CK Ryoo, Y Kim, J Kim 2011 11th International Conference on Control, Automation and Systems, 969-972, 2011 | 45 | 2011 |
Guidance synthesis for evasive maneuver of anti-ship missiles against close-in weapon systems YH Kim, CK Ryoo, MJ Tahk IEEE Transactions on Aerospace and Electronic Systems 46 (3), 1376-1388, 2010 | 35 | 2010 |
Optimal UAV formation guidance laws with timing constraint CK Ryoo, YH Kim, MJ Tahk International journal of systems science 37 (6), 415-427, 2006 | 33 | 2006 |
Missile guidance law estimation using modified interactive multiple model filter J Yun, CK Ryoo Journal of Guidance, Control, and Dynamics 37 (2), 484-496, 2014 | 30 | 2014 |
Integrated guidance and control law with impact angle constraint J Yun, CK Ryoo 2011 11th International Conference on Control, Automation and Systems, 1239-1243, 2011 | 27 | 2011 |
Quaternion based three-dimensional impact angle control guidance law JH Kim, SS Park, KK Park, CK Ryoo IEEE Transactions on Aerospace and Electronic Systems 57 (4), 2311-2323, 2021 | 24 | 2021 |
A missile guidance law based on Sontag's formula to intercept maneuvering targets CK Ryoo, YH Kim, MJ Tahk, KY Choi International Journal of Control, Automation, and Systems 5 (4), 397-409, 2007 | 24 | 2007 |