Satellite attitude control and power tracking with energy/momentum wheels P Tsiotras, H Shen, C Hall Journal of Guidance, Control, and Dynamics 24 (1), 23-34, 2001 | 230 | 2001 |
Time-optimal control of axisymmetric rigid spacecraft using two controls H Shen, P Tsiotras Journal of Guidance, Control, and Dynamics 22 (5), 682-694, 1999 | 196 | 1999 |
Optimal two-impulse rendezvous using multiple-revolution Lambert solutions H Shen, P Tsiotras Journal of Guidance, Control, and Dynamics 26 (1), 50-61, 2003 | 188 | 2003 |
Tracking rigid body motion using thrusters and momentum wheels CD Hall, P Tsiotras, H Shen The Journal of the Astronautical Sciences 50, 311-323, 2002 | 97 | 2002 |
Peer-to-peer refueling for circular satellite constellations H Shen, P Tsiotras Journal of Guidance, Control, and Dynamics 28 (6), 1220-1230, 2005 | 77 | 2005 |
Desensitizing the minimum-fuel powered descent for mars pinpoint landing H Shen, H Seywald, RW Powell Journal of guidance, control, and dynamics 33 (1), 108-115, 2010 | 72 | 2010 |
Optimal scheduling for servicing multiple satellites in a circular constellation H Shen, P Tsiotras AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 4907, 2002 | 56 | 2002 |
Desensitised kalman filtering CD Karlgaard, H Shen IET Radar, Sonar & Navigation 7 (1), 2-9, 2013 | 45 | 2013 |
Using Battin's method to obtain multiple-revolution Lambert's solutions H Shen, P Tsiotras Advances in the Astronautical Sciences 116, 1067-1084, 2003 | 40 | 2003 |
Robust state estimation using desensitized divided difference filter CD Karlgaard, H Shen ISA transactions 52 (5), 629-637, 2013 | 39 | 2013 |
Enhanced gravity tractor technique for planetary defense DD Mazanek, DM Reeves, JB Hopkins, DW Wade, M Tantardini, H Shen IAA Planetary Defense Conference, 2015 | 35 | 2015 |
Optimal scheduling for satellite refuelling in circular orbits H Shen Georgia Institute of Technology, 2003 | 32 | 2003 |
Desensitizing the pin-point landing trajectory on mars H Shen, H Seywald, R Powell AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 6943, 2008 | 27 | 2008 |
Optimal two-impulse Rendezvous between two circular orbits using Multiple-Revolution Lambert's Solutions H Shen, P Tsiotras AIAA Guidance, Navigation, and Control Conference and Exhibit, 4844, 2002 | 20 | 2002 |
Sensitivity reduction of unscented Kalman filter about parameter uncertainties H Shen, CD Karlgaard IET Radar, Sonar & Navigation 9 (4), 374-383, 2015 | 17 | 2015 |
Desensitized optimal filtering C Karlgaard, H Shen AIAA Guidance, Navigation, and Control Conference, 6617, 2011 | 16 | 2011 |
Desensitized unscented Kalman filter about uncertain model parameters HJ Shen, CD Karlgaard Institute of Navigation International Technical Meeting, Newport Beach …, 2012 | 12 | 2012 |
Automation of a Versatile Crane (the LSMS) for Lunar Outpost Construction, Maintenance and Inspection W Doggett, C Roithmayr, J Dorsey, T Jones, B King, M Mikulas, H Shen, ... AIAA SPACE 2009 Conference & Exposition, 6546, 2009 | 10 | 2009 |
Desensitized divided difference filtering for induction motor state estimation CD Karlgaard, H Shen Proceedings of the 2012 44th Southeastern Symposium on System Theory (SSST …, 2012 | 9 | 2012 |
Peer-to-peer refuelling within a satellite constellation part I: zero-cost rendezvous case H Shen, P Tsiotras 42nd IEEE International Conference on Decision and Control (IEEE Cat. No …, 2003 | 9 | 2003 |