Optimal perilune altitude of lunar landing trajectory DH Cho, B Jeong, D Lee, H Bang International Journal of Aeronautical and Space Sciences 10 (1), 67-74, 2009 | 43 | 2009 |
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 | 37 | 2009 |
Efficient initial costates estimation for optimal spiral orbit transfer trajectories design D Lee, H Bang Journal of guidance, control, and dynamics 32 (6), 1943-1947, 2009 | 28 | 2009 |
Flight dynamics and navigation for planetary missions in Korea: past efforts, recent status, and future preparations YJ Song, D Lee, J Bae, YR Kim, SJ Choi Journal of Astronomy and Space Sciences 35 (3), 119-131, 2018 | 20 | 2018 |
Optimal Earth-Moon trajectory design using new initial costate estimation method D Lee, H Bang, HD Kim Journal of guidance, control, and dynamics 35 (5), 1671-1676, 2012 | 19 | 2012 |
Virtual trajectory augmented landing control based on dual quaternion for Lunar Lander JW Kwon, D Lee, H Bang journal of Guidance, Control, and Dynamics 39 (9), 2044-2057, 2016 | 16 | 2016 |
Overview of the Flight Dynamics Subsystem for Korea Pathfinder Lunar Orbiter Mission YJ Song, YR Kim, J Bae, J Park, S Hong, D Lee, DK Kim Aerospace 8 (8), 222, 2021 | 15 | 2021 |
Ground Tracking Support Condition Effect on Orbit Determination for Korea Pathfinder Lunar Orbiter (KPLO) in Lunar Orbit YR Kim, YJ Song, J Park, D Lee, J Bae, SB Hong, DK Kim, SR Lee Journal of Astronomy and Space Sciences 37 (4), 237-247, 2020 | 12 | 2020 |
Energy-efficient swarming flight formation transitions using the improved fair Hungarian algorithm ST Moon, D Lee, D Lee, D Kim, H Bang Sensors 21 (4), 1260, 2021 | 11 | 2021 |
Spacecraft attitude control by combination of various torquers H Leeghim, DH Lee, H Bang, K Lee International journal of systems science 40 (10), 995-1008, 2009 | 10 | 2009 |
Trajectory optimization for a lunar orbiter using a pattern search method SJ Choi, D Lee, IK Kim, JW Kwon, CH Koo, S Moon, C Kim, SY Min, ... Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2017 | 9 | 2017 |
Preliminary design of LUDOLP: the flight dynamics subsystem for the Korea Pathfinder Lunar Orbiter mission YJ Song, D Lee, JH Bae, B Kim, Y Kim, EJ Lee, HJ Kim, S Park 14th International Conference on Space Operations, 2311, 2016 | 9 | 2016 |
Mission orbit design of CubeSat impactor measuring lunar local magnetic field JA Lee, SY Park, Y Kim, J Bae, D Lee, G Ju Journal of Astronomy and Space Sciences 34 (2), 127-138, 2017 | 7 | 2017 |
Potential trajectory design for a lunar CubeSat impactor deployed from a HEPO using only a small separation delta-V YJ Song, D Lee, H Jin, BY Kim Advances in Space Research 59 (2), 619-630, 2017 | 7 | 2017 |
Method and apparatus for contingency guidance of a CMG-actuated spacecraft IM Ross, DH Lee, M Karpenko US Patent 9,038,958, 2015 | 7 | 2015 |
Low thrust, fuel optimal earth escape trajectories design DH Lee, HC Bang Journal of the Korean Society for Aeronautical & Space Sciences 35 (7), 647-654, 2007 | 7 | 2007 |
An antenna tracking profile design for communication with a ground station D Lee, KM Lee, MI Rashed, H Bang International Journal of Aeronautical and Space Sciences 14 (3), 282-295, 2013 | 6 | 2013 |
Optimal Earth Escape Trajectory Using continuation method and costate estimator D Lee, H Bang American Astronomical Society, 2008 | 6 | 2008 |
Orbit transfer trajectory optimization with electric engine DH Cho, D Lee, MJ Tahk 2006 SICE-ICASE International Joint Conference, 4093-4098, 2006 | 6 | 2006 |
Spin-to-spin slew maneuvers under spherically constrained angular acceleration D Lee, YJ Song Advances in Space Research 64 (6), 1274-1285, 2019 | 5 | 2019 |