| Cooperative localization between small UAVs using a combination of heterogeneous sensors W Lee, H Bang, H Leeghim Aerospace science and technology 27 (1), 105-111, 2013 | 66 | 2013 |
| Adaptive attitude control of spacecraft using neural networks H Leeghim, Y Choi, H Bang Acta Astronautica 64 (7-8), 778-786, 2009 | 57 | 2009 |
| Singularity avoidance of control moment gyros by one-step ahead singularity index H Leeghim, H Bang, JO Park Acta Astronautica 64 (9-10), 935-945, 2009 | 50 | 2009 |
| Spacecraft intercept using minimum control energy and wait time H Leeghim Celestial Mechanics and Dynamical Astronomy 115 (1), 1-19, 2013 | 40 | 2013 |
| Singularity avoidance of control moment gyros by predicted singularity robustness: ground experiment H Leeghim, IH Lee, DH Lee, H Bang, JO Park IEEE Transactions on control systems Technology 17 (4), 884-891, 2009 | 35 | 2009 |
| Uncorrelated unscented filtering for spacecraft attitude determination H Leeghim, Y Choi, BA Jaroux Acta Astronautica 67 (1-2), 135-144, 2010 | 31 | 2010 |
| Energy-optimal solution to the lambert problem H Leeghim, BA Jaroux Journal of guidance, control, and dynamics 33 (3), 1008-1010, 2010 | 29 | 2010 |
| Heuristic-based mission planning for an agile earth observation satellite SH Mok, S Jo, H Bang, H Leeghim International Journal of Aeronautical and Space Sciences 20, 781-791, 2019 | 27 | 2019 |
| Feasible angular momentum of spacecraft installed with control moment gyros H Leeghim, J Jin, SH Mok Advances in Space Research 61 (1), 466-477, 2018 | 24 | 2018 |
| Adaptive nonlinear control using input normalized neural networks H Leeghim, IH Seo, H Bang Journal of Mechanical Science and Technology 22, 1073-1083, 2008 | 24 | 2008 |
| Adaptive neural control of spacecraft using control moment gyros H Leeghim, D Kim Advances in Space Research 55 (5), 1382-1393, 2015 | 23 | 2015 |
| Optimal lunar landing trajectory design for hybrid engine DH Cho, D Kim, H Leeghim Mathematical Problems in Engineering 2015, 2015 | 18 | 2015 |
| A cooperative guidance law for target estimation by multiple unmanned aerial vehicles W Lee, H Bang, H Leeghim Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2011 | 17 | 2011 |
| Reaction wheel fault‐tolerant finite‐time control for spacecraft attitude tracking without unwinding D Lee, H Leeghim International Journal of Robust and Nonlinear Control 30 (9), 3672-3691, 2020 | 16 | 2020 |
| A singularity-free steering law of roof array of control moment gyros for agile spacecraft maneuver H Leeghim, CY Lee, J Jin, D Kim International Journal of Control, Automation and Systems 18, 1679-1690, 2020 | 15 | 2020 |
| Angular rate and alignment estimation for gyroless spacecraft by only star trackers H Leeghim, H Bang, CY Lee International Journal of Control, Automation and Systems 16 (5), 2235-2243, 2018 | 15 | 2018 |
| Nonlinear momentum transfer control of a gyrostat with a discrete damper using neural networks IH Seo, H Leeghim, H Bang Acta Astronautica 62 (6-7), 357-373, 2008 | 15 | 2008 |
| A vector measurement-based angular velocity estimation scheme for maneuvering spacecraft S Jo, H Bang, H Leeghim The Journal of the Astronautical Sciences 64, 310-332, 2017 | 11 | 2017 |
| Novel approach to optical profiler with gradient focal point methods H Leeghim, MK Ahn, K Kim Optics Express 20 (21), 23061-23073, 2012 | 11 | 2012 |
| Reorientation of asymmetric rigid body using two controls D Kim, JD Turner, H Leeghim Mathematical Problems in Engineering 2013, 2013 | 10 | 2013 |
