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Which navigational error arises during inertial flight because of the equivalence principle?

A)Coriolis effect calculation errors
B)Accelerometer drift from gravity
C)Integration errors with Kalman filters
D)Gyroscope precession under acceleration

💡 Explanation

The accelerometer cannot distinguish between acceleration and gravity effects, so it experiences accelerometer drift, because of Einstein's equivalence principle, and interprets gravity as a form of acceleration. Therefore, integration of these signals introduces navigational errors, rather than correcting via Coriolis effects within earth's rotation.

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