| 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 | 23 | 2018 |
| Impulsive formation control using orbital energy and angular momentum vector Y Choi, S Mok, H Bang Acta Astronautica 67 (5-6), 613-622, 2010 | 20 | 2010 |
| Sensor-fault tolerant attitude determination using two-stage estimator SY Byeon, SH Mok, H Woo, H Bang Advances in Space Research 63 (11), 3632-3645, 2019 | 17 | 2019 |
| One-step rendezvous guidance for improving observability in bearings-only navigation SH Mok, J Pi, H Bang Advances in Space Research 66 (11), 2689-2702, 2020 | 15 | 2020 |
| Performance comparison of nonlinear estimation techniques in terrain referenced navigation S Mok, M Choi, H Bang 2011 11th International Conference on Control, Automation and Systems, 1244-1249, 2011 | 15 | 2011 |
| Analytical solution for attitude command generation of agile spacecraft SH Mok, H Bang, HS Kim Journal of the Korean Society for Aeronautical & Space Sciences 46 (8), 639-651, 2018 | 12 | 2018 |
| Terrain slope estimation methods using the least squares approach for terrain referenced navigation SH Mok, H Bang International Journal Aeronautical and Space Sciences 14 (1), 85-90, 2013 | 12 | 2013 |
| Terrain referenced navigation for autonomous underwater vehicles SH Mok, H Bang, J Kwon, M Yu Journal of Institute of Control, Robotics and Systems 19 (8), 702-708, 2013 | 10 | 2013 |
| Performance comparison of gyro-based and gyroless attitude estimation for cubesats SH Mok, SY Byeon, H Bang, Y Choi International Journal of Control, Automation and Systems 18, 1150-1160, 2020 | 9 | 2020 |
| Optimal spacecraft rendezvous by minimum velocity change and wait time S Oghim, SH Mok, H Leeghim Advances in Space Research 60 (6), 1188-1200, 2017 | 8 | 2017 |
| Collision avoidance using linear quadratic control in satellite formation flying SH Mok, YH Choi, HC Bang International Journal of Aeronautical and Space Sciences 11 (4), 351-359, 2010 | 8 | 2010 |
| CubeSat altimeter constellation systems: performance analysis and methodology Y Li, P Hoogeboom, PL Dekker, SH Mok, J Guo, C Buck IEEE Transactions on Geoscience and Remote Sensing 60, 1-19, 2021 | 7 | 2021 |
| Optimal multi-target overflight using ground-track adjustment SH Mok, H Bang The Journal of the Astronautical Sciences 68, 150-171, 2021 | 7 | 2021 |
| Vision-based relative navigation using dual quaternion for spacecraft proximity operations Y Na, H Bang, SH Mok International Journal of Aeronautical and Space Sciences 20, 1010-1023, 2019 | 7 | 2019 |
| A performance comparison of nonlinear Kalman filtering based terrain referenced navigation SH Mok, HC Bang, MJ Yu Journal of the Korean Society for Aeronautical & Space Sciences 40 (2), 108-117, 2012 | 7 | 2012 |
| Performance analysis of vision-based terrain referenced navigation S Mok, H Bang, M Yu Journal of Institute of Control, Robotics and Systems 23 (4), 294-299, 2017 | 6 | 2017 |
| A delayed impulse control strategy for spacecraft formations SH Mok, Y Choi, H Bang, H Leeghim The Journal of the Astronautical Sciences 60, 337-365, 2013 | 6 | 2013 |
| Impulsive control of satellite formation flying using orbital period difference S Mok, Y Choi, H Bang IFAC Proceedings Volumes 43 (15), 368-373, 2010 | 6 | 2010 |
| Lunar orbit design of a satellite swarm for radio astronomy SH Mok, J Guo, E Gill, RT Rajan 2020 IEEE Aerospace Conference, 1-9, 2020 | 5 | 2020 |
