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Journal of Applied Mathematics
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Journal of Applied Mathematics
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2014
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Article
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Tab 1
Research Article
An Adaptive Unscented Kalman Filtering Algorithm for MEMS/GPS Integrated Navigation Systems
Table 1
Parameters of sensor errors.
Sensor
Characteristic
Value
MEMS Gyro
Drift
5°/h
MEMS Gyro
Measuring white noise
0.5°/h
MEMS accelerometer
Bias
2 mg
MEMS accelerometer
Measuring white noise
50
g
GPS (position)
Measuring white noise
6 m
GPS (velocity)
Measuring white noise
0.01 m/s