| Quarternion feedback regulator for spacecraft eigenaxis rotations B Wie, H Weiss, A Arapostathis Journal of Guidance, Control, and Dynamics 12 (3), 375-380, 1989 | 707 | 1989 |
| System Characterization of Positive Real Conditions H Weiss, Q Wang, JL Speyer IEEE Trans. on Automatic Control 39 (3), 540-544, 1994 | 108 | 1994 |
| Improved extended Kalman filter design for passive tracking H Weiss, J Moore IEEE Transactions on Automatic Control 25 (4), 807-811, 1980 | 101 | 1980 |
| Quaternion-based rate/attitude tracking system with application to gimbal attitude control H Weiss Journal of Guidance, Control, and Dynamics 16 (4), 609-616, 1993 | 84 | 1993 |
| Desgin of CLOS Guidance System G Hexner, H Weiss Advances in Missile Guidance, Control, and Estimation 47, 527-586, 2012 | 66* | 2012 |
| Recursive Prediction Error Methods for Adaptive Estimation JB Moore, H Weiss 17th IEEE Conference on Decision and Control, 586-591, 1978 | 59 | 1978 |
| On the solution of the discrete-time Lyapunov matrix equation in controllable canonical form R Bitmead, H Weiss IEEE Transactions on Automatic Control 24 (3), 481-482, 1979 | 57 | 1979 |
| Guidance laws in target—Missile—Defender scenario with an aggressive defender I Rusnak, H Weiss, G Hexner IFAC Proceedings Volumes 44 (1), 9349-9354, 2011 | 52 | 2011 |
| New interceptor guidance law integrating time-varying and estimation-delay models T Shima, J Shinar, H Weiss Journal of Guidance, Control, and Dynamics 26 (2), 295-303, 2003 | 50 | 2003 |
| 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 | 48 | 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 |
| LQC guidance law with bounded acceleration command G Hexner, T Shima, H Weiss IEEE Transactions on Aerospace and Electronic Systems 44 (1), 77-86, 2008 | 42 | 2008 |
| Improving the performance of existing missile autopilot using simple adaptive control I Rusnak, H Weiss, I Barkana International Journal of Adaptive Control and Signal Processing 28 (7-8 …, 2014 | 39 | 2014 |
| Method and system for destroying rockets O Golan, H Weiss, I Lupa, R Fishman US Patent App. 10/563,296, 2006 | 39 | 2006 |
| Derivation of formation-flight guidance laws for unmanned air vehicles S Segal, JZ Ben-Asher, H Weiss Journal of Guidance, Control, and Dynamics 28 (4), 733-742, 2005 | 35 | 2005 |
| Almost Passivity and Simple Adaptive Control in Discrete‐Time Systems I Barkana, I Rusnak, H Weiss Asian Journal of Control 16 (4), 947-958, 2014 | 31 | 2014 |
| Missile guidance with constrained terminal body angle I Rusnak, H Weiss, R Eliav, T Shima 2010 IEEE 26-th Convention of Electrical and Electronics Engineers in Israel …, 2010 | 30 | 2010 |
| Missile guidance with constrained intercept body angle I Rusnak, H Weiss, R Eliav, T Shima IEEE Transactions on Aerospace and Electronic Systems 50 (2), 1445-1453, 2014 | 27 | 2014 |
| Improving the performance of existing missile autopilot using simple adaptive control I Rusnak, H Weiss, I Barkana IFAC Proceedings Volumes 44 (1), 6567-6572, 2011 | 26 | 2011 |
| On algorithms for attitude estimation using GPS A Nadler, IY Bar-Itzhack, H Weiss Proceedings of the 39th IEEE Conference on Decision and Control (Cat. No …, 2000 | 26 | 2000 |
Tal ShimaTechnion - Israel Institute of TechnologyПодтвержден адрес электронной почты в домене technion.ac.il
