Accession Number : AD0682461
Title : ABOUT EQUATIONS OF ERRORS OF INERTIAL NAVIGATION SYSTEMS, DETERMINING ARBITRARY CURVILINEAR COORDINATES OF A MOVING OBJECT,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
Personal Author(s) : Andreev, V. D.
Report Date : 19 JUL 1968
Pagination or Media Count : 19
Abstract : The report discusses the perturbed motion of an inertial navigation system, when its elements have instrumental error, and the initial conditions are inaccurate. Derived are equations of errors in the determination of inertial coordinate systems of an object and parameters, characterizing its orientation in space. It is shown, how these equations can be reduced to equations of errors of inertial systems, determining Descartes' coordinates of the object. (Author)
Descriptors : (*INERTIAL NAVIGATION, ERRORS), INSTRUMENTATION, GYROSCOPES, EQUATIONS OF MOTION, PERTURBATION THEORY, TENSOR ANALYSIS, USSR.
Subject Categories : Navigation and Guidance
Distribution Statement : APPROVED FOR PUBLIC RELEASE