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47篇 您的检索式：作者名="Itzhack Y"

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	题名	作者	年代	出处	被引量
1	Optimal Weighted Or thogonalization of Measured Modes显示文摘	BARUCH M ITZHACK Y B	1978	AIIA Journal1978，16，4：	1
2	Unified Approach to Inertial Navigation System Error Modeling显示文摘	Goshen Meskin D Bar Itzhack I Y	1992	Journal Guidance Control and Dynamics1992，15，3：	1
3	Comprehensive evaluation of attitude and orbit estimation using actual earth magnetic field data显示文摘	Deutschmann J Itzhack I Y B	2001	Journal of Guidance Control and Dynamics2001，24，3：	1
4	OptimizedTRIAD algorithm for attitude determination 显示文摘	Itzhack Y Bar - Itzhack and Richard R Harman	1997	Journal ofGuidance Control and Dynamics ( S0731 -5090)1997，20，1：	1
5	Inertial navigation system aided by aircraft dynamics显示文摘	KOIFMAN M BAR ITZHACK I Y	1999	IEEE Transactions on Control Systems Technology1999，7，4：	1
6	Observability analysis of piece-wise constant systems-partⅠ: theory显示文摘	GOSHEN MESKIN D BAR ITZHACK I Y	1992	IEEE Transactions on Aerospace and Electronic Systems1992，28，4：	1
7	Optimal weighted orthogonalization of measured modes显示文摘	Baruch M Bar Itzhack I Y	1978	AIAA J1978，16，4：	1
8	Satellite Autonomous Navigation Based on Magnetic Field Measurements 显示文摘	Gil Shorshi Itzhack Y B	1995	Journal of Guidance Control and Dynamics1995，18，4：	1
9	Observability analysis of piece wise constant system part Ⅰ :Theory 显示文摘	Goshen Meskin D Bar Itzhack I Y	1992	IEEE Transaction on Aerospace and Electronic Systems1992，19，2：	1
10	Navigation computation in terrestrial strapdown inertial navigation system 显示文摘	I Y Bar - Itzhack	1977	IEEE Transactions on Aerospace and Electronic System1977，13，6：	1
11	Unified approach to inertial navigation system error modeling 显示文摘	Goshen Meskin D Bar Itzhack I Y	1992	AIAA Journal of Guidance Control and Dynamics1992，15，3：	1
12	Optimal weighted orthogonalization of measured modes显示文摘	Bar Itzhack I Y	1978	AIAA Journal1978，16，：	1
13	In-apace calibration of a gyro quadruplet显示文摘	Itzhack Y Bar-Itzhack harman Richard R	2001	AIAA Guidance Navigation and Control Conference and Exhibit AIAA-2001-41522001，2001，：	1
14	Azimuth observability enhance ment during inertial navigation system in-flight align ment显示文摘	Itzhack Y Boaz P	1980	J Guidance and Control1980，3，4：	1
15	New method for extracting the quaternion from a rotation matrix显示文摘	BARITZHACK I Y	2000	Journal of Guidance and2000，23，6：	1
16	Observability analysis of piece-wise constant system,part Ⅱ:application to inertial navigation in-flight alignment显示文摘	Goshen Meskin D Bar Itzhack Ⅰ Y	1992	IEEE Transactions on Aerospace and Electronics Systems1992，28，4：	1
17	Unified approach to inertial navigation system error modeling显示文摘	Bar Itzhack I Y Goshen Meskin D	1992	Journal of Guidance Control and Dynamics1992，15，3：	1
18	Unified approach to inertial navigation system error modeling 显示文摘	Go shenMesk in D Bar Itzhack I Y	1992	Journal Guidance Control and Dynamics1992，15，3：	1
19	Optimal weighted orthogonalization of measured modes 显示文摘	Baruch M Bar Itzhack I Y	1978	AIAA Journal1978，16，4：	1
20	Unified approach to inertial navigation system error modeling显示文摘	Goshen-Meskin D Bar Itzhack I Y	1992	AIAA Journal of Guidance Control and Dynamics1992，15，3：	1

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