Takip et
Yaakov Oshman
Yaakov Oshman
Professor of Aerospace Engineering, Technion - Israel Institute of Technology
technion.ac.il üzerinde doğrulanmış e-posta adresine sahip - Ana Sayfa
Başlık
Alıntı yapanlar
Alıntı yapanlar
Yıl
Novel quaternion Kalman filter
D Choukroun, IY Bar-Itzhack, Y Oshman
IEEE Transactions on Aerospace and Electronic Systems 42 (1), 174-190, 2006
4932006
Averaging quaternions
FL Markley, Y Cheng, JL Crassidis, Y Oshman
Journal of Guidance, Control, and Dynamics 30 (4), 1193-1197, 2007
4572007
Optimization of observer trajectories for bearings-only target localization
Y Oshman, P Davidson
IEEE Transactions on Aerospace and Electronic Systems 35 (3), 892-902, 1999
4481999
Attitude determination from vector observations: Quaternion estimation
IY Bar-Itzhack, Y Oshman
IEEE Transactions on Aerospace and Electronic Systems, 128-136, 1985
3881985
Attitude estimation from vector observations using a genetic-algorithm-embedded quaternion particle filter
Y Oshman, A Carmi
Journal of Guidance, Control, and Dynamics 29 (4), 879-891, 2006
1322006
Optimal sensor selection strategy for discrete-time state estimators
Y Oshman
IEEE Transactions on Aerospace and Electronic Systems 30 (2), 307-314, 1994
1181994
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
Efficient multiple model adaptive estimation in ballistic missile interception scenarios
T Shima, Y Oshman, J Shinar
Journal of Guidance, Control, and Dynamics 25 (4), 667-675, 2002
862002
Integrated estimation/guidance design approach for improved homing against randomly maneuvering targets
J Shinar, V Turetsky, Y Oshman
Journal of Guidance, Control, and Dynamics 30 (1), 154-161, 2007
712007
Spacecraft angular rate estimation from magnetometer data only using an analytic predictor
P Tortora, Y Oshman, F Santoni
Journal of Guidance, Control, and Dynamics 27 (3), 365-373, 2004
662004
Differential-game-based guidance law using target orientation observations
Y Oshman, DA Rad
IEEE Transactions on Aerospace and Electronic Systems 42 (1), 316-326, 2006
642006
Adaptive particle filtering for spacecraft attitude estimation from vector observations
A Carmi, Y Oshman
Journal of Guidance, Control, and Dynamics 32 (1), 232-241, 2009
612009
Eigenfactor solution of the matrix Riccati equation--A continuous square root algorithm
Y Oshman, I Bar-Itzhack
IEEE Transactions on automatic Control 30 (10), 971-978, 1985
541985
Spacecraft attitude rate estimation from geomagnetic field measurements
ML Psiaki, Y Oshman
Journal of Guidance, Control, and Dynamics 26 (2), 244-252, 2003
512003
Sequential attitude and attitude-rate estimation using integrated-rate parameters
Y Oshman, FL Markley
Journal of Guidance, Control, and Dynamics 22 (3), 385-394, 1999
511999
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
472006
Optimal tuning of a Kalman filter using genetic algorithms
Y Oshman, I Shaviv
AIAA Guidance, Navigation, and Control Conference and Exhibit, 4558, 2000
462000
Using a multiple-model adaptive estimator in a random evasion missile/aircraft encounter
Y Oshman, J Shinar, SA Weizman
Journal of Guidance, Control, and Dynamics 24 (6), 1176-1186, 2001
432001
Distributed structural control using multilayered piezoelectric actuators
H Cudney, D INMAN, Y Oshman
31st structures, structural dynamics and materials conference, 1088, 1990
421990
Cooperative interception in a multi-missile engagement
V Shaferman, Y Oshman
AIAA guidance, navigation, and control conference, 5783, 2009
402009
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