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Daero Lee, Ph.D. - Publications

Affiliations: 
2009 Missouri University of Science and Technology, Rolla, MO, United States 
Area:
Aerospace Engineering
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26 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2020 Lee D, Sim J, Han K, Kim C, Koh GO. Angle-of-Attack Command Longitudinal Control for Supersonic Advanced Trainer Aircraft International Journal of Aeronautical and Space Sciences. 1-9. DOI: 10.1007/S42405-020-00279-2  0.408
2020 Lee D, Leeghim H. Reaction wheel fault‐tolerant finite‐time control for spacecraft attitude tracking without unwinding International Journal of Robust and Nonlinear Control. 30: 3672-3691. DOI: 10.1002/Rnc.4957  0.358
2017 Lee D, Vukovich G, Lee R. Robust Adaptive Unscented Kalman Filter for Spacecraft Attitude Estimation Using Quaternion Measurements Journal of Aerospace Engineering. 30: 4017009. DOI: 10.1061/(Asce)As.1943-5525.0000718  0.365
2017 Lee D, Vukovich G, Gui H. Adaptive variable-structure finite-time mode control for spacecraft proximity operations with actuator saturation Advances in Space Research. 59: 2473-2487. DOI: 10.1016/J.Asr.2017.02.029  0.458
2017 Lee D, Vukovich G, Lee R. Robust unscented Kalman filter for nanosat attitude estimation International Journal of Control Automation and Systems. 15: 2161-2173. DOI: 10.1007/S12555-016-0498-4  0.349
2017 Lee D, Vukovich G. Almost global finite-time stabilization of spacecraft formation flying with decentralized collision avoidance International Journal of Control Automation and Systems. 15: 1167-1180. DOI: 10.1007/S12555-016-0239-8  0.387
2017 Lee D. Nonlinear disturbance observer-based robust control of attitude tracking of rigid spacecraft Nonlinear Dynamics. 88: 1317-1328. DOI: 10.1007/S11071-016-3312-1  0.448
2016 Lee D, Vukovich G. Adaptive finite-time control for spacecraft hovering over an asteroid Ieee Transactions On Aerospace and Electronic Systems. 52: 1183-1196. DOI: 10.1109/Taes.2015.140822  0.414
2016 Lee D, Vukovich G. Robust adaptive terminal sliding mode control on SE(3) for autonomous spacecraft rendezvous and docking Nonlinear Dynamics. 83: 2263-2279. DOI: 10.1007/S11071-015-2479-1  0.473
2015 Lee D, Sanyal AK, Butcher EA. Asymptotic tracking control for spacecraft formation flying with decentralized collision avoidance Journal of Guidance, Control, and Dynamics. 38: 587-600. DOI: 10.2514/1.G000101  0.442
2015 Lee D, Sanyal A, Butcher E, Scheeres D. Finite-time control for spacecraft body-fixed hovering over an asteroid Ieee Transactions On Aerospace and Electronic Systems. 51: 506-520. DOI: 10.1109/Taes.2014.140197  0.382
2015 Lee D. Spacecraft Coupled Tracking Maneuver Using Sliding Mode Control with Input Saturation Journal of Aerospace Engineering. 28: 4014136. DOI: 10.1061/(Asce)As.1943-5525.0000473  0.439
2015 Lee D, Bang H, Butcher EA, Sanyal AK. Kinematically coupled relative spacecraft motion control using the state-dependent riccati equation method Journal of Aerospace Engineering. 28. DOI: 10.1061/(Asce)As.1943-5525.0000436  0.414
2015 Lee D, Vukovich G. Adaptive sliding mode control for spacecraft body-fixed hovering in the proximity of an asteroid Aerospace Science and Technology. 46: 471-483. DOI: 10.1016/J.Ast.2015.09.001  0.452
2015 Lee D, Vukovich G. Kinematically coupled spacecraft relative motion without attitude synchronization assumption Aerospace Science and Technology. 45: 316-323. DOI: 10.1016/J.Ast.2015.05.020  0.367
2014 Lee D, Bang H, Butcher EA, Sanyal AK. Nonlinear output tracking and disturbance rejection for autonomous close-range rendezvous and docking of spacecraft Transactions of the Japan Society For Aeronautical and Space Sciences. 57: 225-237. DOI: 10.2322/Tjsass.57.225  0.439
2014 Lee D, Butcher EA, Sanyal AK. Optimal interior Earth-Moon Lagrange point transfer trajectories using mixed impulsive and continuous thrust Aerospace Science and Technology. 39: 281-292. DOI: 10.1016/J.Ast.2014.09.016  0.351
2014 Lee D, Sanyal AK, Butcher EA, Scheeres DJ. Almost global asymptotic tracking control for spacecraft body-fixed hovering over an asteroid Aerospace Science and Technology. 38: 105-115. DOI: 10.1016/J.Ast.2014.07.013  0.461
2012 No TS, Lee JM, Jeon GE, Lee D, Kim G. A Study on Earth-Moon Transfer Orbit Design International Journal of Aeronautical and Space Sciences. 13: 106-116. DOI: 10.5139/Ijass.2012.13.1.106  0.328
2012 Lee D, Cochran JE, No TS. Robust Position and Attitude Control for Spacecraft Formation Flying Journal of Aerospace Engineering. 25: 436-447. DOI: 10.1061/(Asce)As.1943-5525.0000146  0.478
2012 Lee D, Cochran JE, No TS. Orbital dispersion and Earth-impact probability analysis for fragmented asteroids Aerospace Science and Technology. 22: 24-30. DOI: 10.1016/J.Ast.2011.05.009  0.328
2011 Lee D, No T, Lee J, Jeon G. A Parametric Study on Optimal Earth-Moon Transfer Trajectory Design Using Mixed Impulsive and Continuous Thrust Journal of the Korean Society For Aeronautical & Space Sciences. 39: 1021-1032. DOI: 10.5139/Jksas.2011.39.11.1021  0.304
2011 Lee D, Pernicka H. Integrated System for Autonomous Proximity Operations and Docking International Journal of Aeronautical and Space Sciences. 12: 43-56. DOI: 10.5139/Ijass.2011.12.1.43  0.634
2011 Lee D, Pernicka H. Vision-Based Relative State Estimation Using the Unscented Kalman Filter International Journal of Aeronautical and Space Sciences. 12: 24-36. DOI: 10.5139/Ijass.2011.12.1.24  0.618
2010 Lee D, Pernicka H. Optimal Control for Proximity Operations and Docking International Journal of Aeronautical and Space Sciences. 11: 206-220. DOI: 10.5139/Ijass.2010.11.3.206  0.653
2007 Lee D, Cochran JE, Jo JH. Solutions to the variational equations for relative motion of satellites Journal of Guidance, Control, and Dynamics. 30: 669-678. DOI: 10.2514/1.24373  0.331
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