Prominent among the commonly encountered gyro-stabilized assemblies used in guidance and tracking are those which are eddy-current torqued. Although eddy-current-torquecd lead- computing gunsights, which use spinning mirrors, have been well known for thirty years, it has been difficult to find an analysis of the torques developed by the precession mechanism. In this paper a model configuration of the torquer is presented. The total gyro dynamics are then determined by including these torque terms in the model presented in the preceding paper.
Dynamics of an Eddy-Current-Torqued Gyro-Stabilized Assembly
IEEE Transactions on Aerospace and Electronic Systems ; AES-10 , 1 ; 123-127
1974-01-01
455536 byte
Article (Journal)
Electronic Resource
English
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