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Criterion for Angular Noise in Star-Lock Systems

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1 Author(s)
Sandeman, E.K. ; Guided Weapons Division, English Electric Aviation, Ltd., British Aircraft Corporation, Ltd., Luton Airport, Bedfordshire, England.

This paper shows that, if the signal-to-noise power ratio (S/N) is found for any steady deviation ¿ of a parameter from its required value, then in a closed-loop linear servo system, the actual rms variation of the parameter from its required value due to noise cannot exceed the rms value:

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Aerospace and Navigational Electronics, IRE Transactions on  (Volume:ANE-9 ,  Issue: 1 )