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haim weiss
haim weiss
Research Fellow, Rafael
Verified email at rafael.co.il
Title
Cited by
Cited by
Year
Quarternion feedback regulator for spacecraft eigenaxis rotations
B Wie, H Weiss, A Arapostathis
Journal of Guidance, Control, and Dynamics 12 (3), 375-380, 1989
6871989
System Characterization of Positive Real Conditions
H Weiss, Q Wang, JL Speyer
IEEE Trans. on Automatic Control 39 (3), 540-544, 1994
1071994
Improved extended Kalman filter design for passive tracking
H Weiss, J Moore
IEEE Transactions on Automatic Control 25 (4), 807-811, 1980
1001980
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
801993
Desgin of CLOS Guidance System
G Hexner, H Weiss
Advances in Missile Guidance, Control, and Estimation 47, 527-586, 2012
68*2012
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
601979
Recursive Prediction Error Methods for Adaptive Estimation
JB Moore, H Weiss
17th IEEE Conference on Decision and Control, 586-591, 1978
571978
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
502011
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
502003
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
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
412008
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
392014
Method and system for destroying rockets
O Golan, H Weiss, I Lupa, R Fishman
US Patent App. 10/563,296, 2006
352006
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
342005
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
312014
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
302010
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
262014
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
252011
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
242000
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