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Haijun Shen
Haijun Shen
Omitron, Inc., Beltsville, MD
Verified email at omitron.com - Homepage
Title
Cited by
Cited by
Year
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
2302001
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
1941999
Optimal two-impulse rendezvous using multiple-revolution Lambert solutions
H Shen, P Tsiotras
Journal of Guidance, Control, and Dynamics 26 (1), 50-61, 2003
1852003
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
962002
Peer-to-peer refueling for circular satellite constellations
H Shen, P Tsiotras
Journal of Guidance, Control, and Dynamics 28 (6), 1220-1230, 2005
732005
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
682010
Optimal scheduling for servicing multiple satellites in a circular constellation
H Shen, P Tsiotras
AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 4907, 2002
532002
Desensitised kalman filtering
CD Karlgaard, H Shen
IET Radar, Sonar & Navigation 7 (1), 2-9, 2013
452013
Robust state estimation using desensitized divided difference filter
CD Karlgaard, H Shen
ISA transactions 52 (5), 629-637, 2013
392013
Using Battin's method to obtain multiple-revolution Lambert's solutions
H Shen, P Tsiotras
Advances in the Astronautical Sciences 116, 1067-1084, 2003
392003
Enhanced gravity tractor technique for planetary defense
DD Mazanek, DM Reeves, JB Hopkins, DW Wade, M Tantardini, H Shen
IAA Planetary Defense Conference, 2015
352015
Optimal scheduling for satellite refuelling in circular orbits
H Shen
Georgia Institute of Technology, 2003
312003
Desensitizing the pin-point landing trajectory on mars
H Shen, H Seywald, R Powell
AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 6943, 2008
262008
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
202002
Sensitivity reduction of unscented Kalman filter about parameter uncertainties
H Shen, CD Karlgaard
IET Radar, Sonar & Navigation 9 (4), 374-383, 2015
162015
Desensitized optimal filtering
C Karlgaard, H Shen
AIAA Guidance, Navigation, and Control Conference, 6617, 2011
152011
Desensitized unscented Kalman filter about uncertain model parameters
HJ Shen, CD Karlgaard
Institute of Navigation International Technical Meeting, Newport Beach …, 2012
132012
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
92012
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
92009
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
92003
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