| Novel quaternion Kalman filter D Choukroun, IY Bar-Itzhack, Y Oshman IEEE Transactions on Aerospace and Electronic Systems 42 (1), 174-190, 2006 | 503 | 2006 |
| Novel methods for attitude determination using vector observations D Choukroun Technion-Israel Institute of Technology, Faculty of Aerospace Engineering, 2003 | 129 | 2003 |
| Optimal-REQUEST algorithm for attitude determination D Choukroun, IY Bar-Itzhack, Y Oshman Journal of Guidance, Control, and Dynamics 27 (3), 418-425, 2004 | 110 | 2004 |
| 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 | 55 | 2015 |
| 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 | 47 | 2006 |
| 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 | 45* | 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 | 39 | 2016 |
| A new contact dynamics model tool for hardware-in-the-loop docking simulation M Zebenay, R Lampariello, T Boge, D Choukroun | 29 | 2012 |
| 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 | 25 | 2017 |
| 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 | 22 | 2016 |
| Modeling and stability analysis of a hybrid docking simulator MM Zebenay, T Boge, D Choukroun AIAA Guidance, Navigation, and Control (GNC) Conference, 4520, 2013 | 21 | 2013 |
| 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 | 18 | 2012 |
| 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 | 17 | 2002 |
| Novel results on quaternion modeling and estimation from vector observations D Choukroun AIAA Guidance, Navigation, and Control Conference, 6315, 2009 | 12 | 2009 |
| Attitude control system of the Delfi-n3Xt satellite J Reijneveld, D Choukroun Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection …, 2013 | 11 | 2013 |
| Attitude control of the Delfi-n3Xt satellite J Reijneveld, D Choukroun AIAA Guidance, Navigation, and Control Conference, 5043, 2012 | 11 | 2012 |
| Process noise covariance design in Kalman filtering via bounds optimization M Salvoldi, D Choukroun IEEE Transactions on Automatic Control 64 (2), 834-840, 2018 | 10 | 2018 |
| 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 | 10 | 2014 |
| Robust nonlinear H∞ output-feedback for spacecraft attitude control A Capua, A Shapiro, D Choukroun AIAA guidance, navigation, and control conference, 0455, 2014 | 10 | 2014 |
| Optimized state-dependent Riccati equation method for spacecraft attitude estimation and control L Haim, D Choukroun AIAA Guidance, Navigation, and Control Conference, 4557, 2012 | 8 | 2012 |
