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Gyroscopes used in inertial navigation
Authors:A. W. Lawrence
Affiliation:British Aircraft Corporation, Guided Weapons Division , Stevenage
Abstract:This article first defines inertial navigation and then considers a typical accelerometer. The basic law of gyroscopics is then derived, and the distinction between free, rate, and integrating gyroscopes is made. The design of the components of a gyro is discussed; ball and gas bearings for gyro wheels, gimbal suspensions (both floated and unfloated), and types of pickoff and torquer are mentioned, also a component which combines both in one unit. Future types of gyroscope are discussed, among them the electrostatic, cryogenic, laser and nuclear spin gyroscopes.
Keywords:
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