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Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias

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Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias

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Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias

Product Description: Product Description The inertial angle rate sensor we offer employs the optical Sagnac effect as the fundamental principle to measure the rotational angular velocity along its ...

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Aero-grade FOG sensor

FOG sensor for aircraft navigation system

aircraft navigation system FOG sensor

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