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Journal of Sensors
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2018
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Article
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Tab 4
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Research Article
A Preferable Airborne Integrated Navigation Method Based on INS and GPS
Table 4
Error values of IMU.
Gyroscope errors
Bias
1°/h
Scale factor
300 ppm
Misalignment
40
Accelerometer errors
Bias
500
μ
g
Scale factor
300 ppm
Misalignment
40