Fiber Optic Gyro Q&A; Sagnac Effect: BOTH Rectilinear & Angular Motion

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Fiber Optic Gyro Q&A; Sagnac Effect: BOTH Rectilinear & Angular Motion

Thanks to Rick, 7th Day Truth Seeker, for this compilation in efforts of providing a better understanding of LASER Interferometry and its role in proving the rotating aether and the stationary Earth.
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Paper One:
The Sagnac Effect Falsifies Special Relativity Theory
https://www.researchgate.net/publication/315759336_The_Sagnac_Effect_Falsifies_Special_Relativity_Theory

Paper Two:
Error in Michelson Morley Experiment
http://vixra.org/pdf/1902.0285v1.pdf

Paper Three:
Generalize Sagnac Effect
https://www.researchgate.net/publication/8195374_Generalized_Sagnac_Effect

These scientists demonstrate and accurately measure rectilinear motion due to the Sagnac Effect, proving that the Sagnac Effect is not confined to rotational, angular velocity.

The first four tests are 1 minute 30 second tests, with the y axis pointed in each of the four cardinal directions. With these tests, the x and y axes’ maximums and nulls are illustrated. These tests also show the nature of the registered z axis rotation, which should remain constant for each of the four tests. The yaw rotation for my latitude expected after 1.5 minutes is 0.245°. Two tests were high and two tests were low.

The last two tests are both one hour tests. One test has the gyro stationary, and the other test rotates the gyro CCW at 7.5°/hr. The tests are presented in parallel on the screen. The x and y axis readings are irrelevant for this test. We are testing z axis (yaw) readings for the tests.

For the stationary test, the z axis rotation for the globe model for my latitude is expected to be 15 x sine 40.87 = 9.81°. Tested yaw result was 8.45°.

The CCW rotation test registered 16.046° in one hour. Subtracting the measured stationary (aether) drift: 16.046° – 8.447° = 7.599° Thus, the measured result was 101.32% of the expected 7.5° CCW rotation.

In actual practice, the gyro’s contribution to an Inertial Measurement Unit (IMU) is its accuracy in registering high velocity motion. The slow aether drift of the gyro is removed by the sensor fusion software. There are no accelerometers, or magnetometers, or GPS input in the tested device…and no sensor fusion combining the gyroscope data with those other sensor readings.
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