Accession Number : AD0700605
Title : DESIGNING DIFFERENTIATING AND INTEGRATING GYROSCOPES AND ACCELEROMETERS,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
Personal Author(s) : Nikitin, E. A. ; Balashova, A. A.
Report Date : 21 OCT 1969
Pagination or Media Count : 268
Abstract : The book covers the fundamentals of analysis and designing of differentiating and integrating gyroscopes and accelerometers and an analysis of their errors under different operating conditions is given. Simple calculation formulas for determination of the basic parameters of these instruments and also their instrumental and methodical errors are given. Depending upon the assignment of the instrument, requirements for static, dynamic, and accuracy characteristics are shown. Much attention is given description of the physical essence and causes of appearance of the examined errors. (Author)
Descriptors : *ACCELEROMETERS, *ATTITUDE CONTROL SYSTEMS, *GYROSCOPES, INERTIAL GUIDANCE, AIRCRAFT, GUIDED MISSILES, EQUATIONS OF MOTION, GYRO STABILIZERS, DETECTORS, TEXTBOOKS, USSR.
Subject Categories : Air Navigation and Guidance
Distribution Statement : APPROVED FOR PUBLIC RELEASE