Results 141 to 150 of about 5,143 (196)
Data Fusion of Dual Foot-Mounted INS Based on Human Step Length Model. [PDF]
Sensors (Basel)Chen J, Liu G, Guo M.
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Enhancing Pure Inertial Navigation Accuracy through a Redundant High-Precision Accelerometer-Based Method Utilizing Neural Networks. [PDF]
Sensors (Basel)He Q, Yu H, Liang D, Yang X.
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A Kalman Filtering Algorithm for Measurement Interruption Based on Polynomial Interpolation and Taylor Expansion. [PDF]
Entropy (Basel)Cheng J, Wang Z, Qi B, Wang H.
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Fiber Optic Gyro Random Error Suppression Based on Dual Adaptive Kalman Filter. [PDF]
Micromachines (Basel)Li H +5 more
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Experimental Research on Shipborne SINS Rapid Mooring Alignment with Variance-Constraint Kalman Filter and GNSS Position Updates. [PDF]
Sensors (Basel)Fan Z, Chai H, Liang X, Wang H.
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IMU Auto-Calibration Based on Quaternion Kalman Filter to Identify Movements of Dairy Cows. [PDF]
Sensors (Basel)Muñoz-Poblete C +3 more
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Saint Petersburg International Conference on Integrated Navigation Systems, 2023 The emergency operation mode of the SINS500NS inertial satellite navigation system associated with the loss of flight and navigation information is considered.
А. В. Чернодаров +3 more
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2023 International Conference on IoT, Communication and Automation Technology (ICICAT), 2023 Strapdown Inertial Navigation System (SINS) is a critical technology for aircraft, ships, vehicles, and rockets to navigate and position themselves. For proper navigational information to be obtained, SINS must first be aligned.
Ankit Vani, Sweta Tripathi, Neeraj Gupta
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