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This paper presents an overview of the development of inertial components, starting with early rocket guidance using spinning mass components through the development of competent munitions using MEMS sensors. It is a compilation of information on evolving gyroscope and accelerometer use in specific system applications, rather than on the sensor development itself. It shows how the component technology changed over the years in the areas of aircraft navigation, submarine inertial navigation, intercontinental and submarine-launched ballistic missile guidance, space systems, and tactical missiles and munitions. Where possible, the description is chronologically based.

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