Results 321 to 330 of about 4,780 (347)
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International Symposium on Microelectronics, 2011
Sensors in Motion Inc. is developing a navigation grade 6 DOF MEMS INS using its proprietary and patented technologies. The military is investing in INS and IMU technology which can answer its needs as well as provide the baseline for hundreds of other DOD and commercial applications which need a C-swap sensitive utility.
D. DeRoo +5 more
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Sensors in Motion Inc. is developing a navigation grade 6 DOF MEMS INS using its proprietary and patented technologies. The military is investing in INS and IMU technology which can answer its needs as well as provide the baseline for hundreds of other DOD and commercial applications which need a C-swap sensitive utility.
D. DeRoo +5 more
openaire +1 more source
Instrumentation Science & Technology, 2012
Due to the advantages of small size and low cost, micro-electro-mechanical system (MEMS) inertial navigation systems (INS) show good prospects for use as a part of measurement-while-drilling (MWD) equipment to guarantee proper directional drilling procedure. Since current MEMS sensors have inaccurate measurements, an update aiding solution is developed
Rong Li +5 more
openaire +1 more source
Due to the advantages of small size and low cost, micro-electro-mechanical system (MEMS) inertial navigation systems (INS) show good prospects for use as a part of measurement-while-drilling (MWD) equipment to guarantee proper directional drilling procedure. Since current MEMS sensors have inaccurate measurements, an update aiding solution is developed
Rong Li +5 more
openaire +1 more source
With the advancement of sensor technology, the disablement in 2000 of selective availability (a corrupting signal superimposed GPS broadcast signals to reduce accuracy), and the decreasing costs of computational equipment, a large number of navigational projects are becoming feasible.
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1994
Abstract : The purpose of this research is to compare the effects of two filtering routines which may be used to integrate Inertial Navigation System (INS) and Global Positioning System (GPS) data to determine certain state vector elements. The two filtering routines are: 1) the ordinary Kalman Filter, and 2) a Two-Stage Least- Squares Procedure, which
openaire +1 more source
Abstract : The purpose of this research is to compare the effects of two filtering routines which may be used to integrate Inertial Navigation System (INS) and Global Positioning System (GPS) data to determine certain state vector elements. The two filtering routines are: 1) the ordinary Kalman Filter, and 2) a Two-Stage Least- Squares Procedure, which
openaire +1 more source
Inertial-Based Integration With Transformed INS Mechanization in Earth Frame
IEEE/ASME Transactions on Mechatronics, 2022Lubin Chang, Fangjun Qin
exaly
GPS data correction using encoders and inertial navigation system (INS) sensors
2011S.A. Berrabah, Y. Baudoin
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Improved polar inertial navigation algorithm based on pseudo INS mechanization
Aerospace Science and Technology, 2018Guangchun Li, Yanbin Gao, Shutong Li
exaly
Inertial Navigation System of Pipeline Inspection Gauge
IEEE Transactions on Control Systems Technology, 2020Wasim M F Al-Masri +2 more
exaly

