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Daniel Choukroun
Daniel Choukroun
Senior Lecturer (Assistant Professor) Mechanical Engineering Dept. Ben-Gurion University
Verified email at bgu.ac.il
Title
Cited by
Cited by
Year
Novel quaternion Kalman filter
D Choukroun, IY Bar-Itzhack, Y Oshman
IEEE Transactions on Aerospace and Electronic Systems 42 (1), 174-190, 2006
4922006
Novel methods for attitude determination using vector observations
D Choukroun
Technion-Israel Institute of Technology, Faculty of Aerospace Engineering, 2003
1272003
Optimal-REQUEST algorithm for attitude determination
D Choukroun, IY Bar-Itzhack, Y Oshman
Journal of Guidance, Control, and Dynamics 27 (3), 418-425, 2004
1092004
Analytical and experimental stability investigation of a hardware-in-the-loop satellite docking simulator
M Zebenay, T Boge, R Krenn, D Choukroun
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2015
532015
Kalman filtering for matrix estimation
D Choukroun, H Weiss, IY Bar-Itzhack, Y Oshman
IEEE Transactions on Aerospace and Electronic Systems 42 (1), 147-159, 2006
462006
Direction cosine matrix estimation from vector observations using a matrix Kalman filter
D Choukroun, H Weiss, IY Bar-Itzhack, Y Oshman
IEEE Transactions on Aerospace and Electronic Systems 46 (1), 61-79, 2010
44*2010
Geostationary satellite station-keeping using convex optimization
FJ De Bruijn, S Theil, D Choukroun, E Gill
Journal of Guidance, Control, and Dynamics 39 (3), 605-616, 2016
332016
A new contact dynamics model tool for hardware-in-the-loop docking simulation
M Zebenay, R Lampariello, T Boge, D Choukroun
262012
Relative navigation in asteroid missions using dual quaternion filtering
B Razgus, E Mooij, D Choukroun
journal of Guidance, Control, and Dynamics 40 (9), 2151-2166, 2017
242017
Modeling and stability analysis of a hybrid docking simulator
MM Zebenay, T Boge, D Choukroun
AIAA Guidance, Navigation, and Control (GNC) Conference, 4520, 2013
212013
Collocation of geostationary satellites using convex optimization
FJ De Bruijn, S Theil, D Choukroun, E Gill
Journal of Guidance, Control, and Dynamics 39 (6), 1303-1313, 2016
202016
Quaternion estimation from vector observations using a matrix Kalman filter
D Choukroun, H Weiss, IY Bar-Itzhack, Y Oshman
IEEE Transactions on Aerospace and Electronic Systems 48 (4), 3133-3158, 2012
182012
State-dependent pseudo-linear filters for spacecraft attitude and rate estimation
I Bar-Itzhack, R Harman, D Choukroun
AIAA Guidance, Navigation, and Control Conference and Exhibit, 4461, 2002
172002
Novel results on quaternion modeling and estimation from vector observations
D Choukroun
AIAA Guidance, Navigation, and Control Conference, 6315, 2009
132009
Robust nonlinear H∞ output-feedback for spacecraft attitude control
A Capua, A Shapiro, D Choukroun
AIAA guidance, navigation, and control conference, 0455, 2014
102014
Attitude control system of the Delfi-n3Xt satellite
J Reijneveld, D Choukroun
Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection …, 2013
102013
Attitude control of the Delfi-n3Xt satellite
J Reijneveld, D Choukroun
AIAA Guidance, Navigation, and Control Conference, 5043, 2012
102012
Space-indexed control for aircraft vertical guidance with time constraint
H Bouadi, F Mora-Camino, D Choukroun
Journal of Guidance, Control, and Dynamics 37 (4), 1103-1113, 2014
92014
Process noise covariance design in Kalman filtering via bounds optimization
M Salvoldi, D Choukroun
IEEE Transactions on Automatic Control 64 (2), 834-840, 2018
82018
Optimized state-dependent Riccati equation method for spacecraft attitude estimation and control
L Haim, D Choukroun
AIAA Guidance, Navigation, and Control Conference, 4557, 2012
82012
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