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Operation was relatively simple: a pilot or flight engineer would enter the individual waypoints by their latitude and longitude points and then the pilot or engineer would enter the starting location in latitude and longitude. The system used spinning mass gyroscopes and proof-mass accelerometers to
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Carousel IV consisted of an inertial measurement unit (IMU) as its position reference, a digital computer to compute the navigation solution, and a control panel mounted in an aircraft's cockpit. It was used for long over water and over the North Pole aircraft navigation. Many aircraft were equipped
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The
Carousel IV system derives its name from the fact that the inertial reference platform was rotated 360° every 60 seconds as a technique to reduce drift and increase accuracy by countering systematic errors. Low drift operation was aided by maintaining the gyroscopes and accelerometers at a
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constant temperature of 60 °C. The elevated temperature was maintained whenever the system was switched on in either the 'Standby', 'Align', 'Navigate' or 'Attitude' mode, as selected on the
Control Display Unit (CDU).
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measure movement from the start point. An involved calculation followed by sampling those sensors to determine a current position relative to the surface of the Earth.
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197:"Plotting LOPs eight miles high - Ocean Navigator"
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