ABOUT EQUATIONS OF ERRORS OF INERTIAL NAVIGATION SYSTEMS, DETERMINING ARBITRARY CURVILINEAR COORDINATES OF A MOVING OBJECT,

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)

Document Details

Document Type
Technical Report
Publication Date
Jul 19, 1968
Accession Number
AD0682461

Entities

People

  • V. D. Andreev

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Coordinate Systems
  • Equations
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Navigation
  • Navigational Equipment
  • Orientation (Direction)
  • World Geodetic System

Fields of Study

  • Physics

Readers

  • Approximation Theory.
  • Computer Vision.
  • Fluid Dynamics.

Technology Areas

  • Space
  • Space - Space Objects