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Inertial navigation systems analysis.This volume offers the avionic systems engineer a fundamental exposition of the mechanization and error analysis of inertial navigation systems. While the material is applicable to spacecraft and undersea navigation, emphasis is placed upon terrestrial applications on or slightly above the earth's surface. As a result, practical considerations are geared toward those aircraft navigation systems of particular current interest. Extensive use is made of perturbation techniques to develop linearized system equations, whose solutions closely approximate those obtained by nonlinear differential equations. A unified error analysis technique is developed that is applicable to virtually all system configurations. The technique provides a greatly simplified method for comparing the performance of competing system configurations.
Document ID
19720034278
Acquisition Source
Legacy CDMS
Document Type
Book
Authors
Britting, K. R.
(MIT Cambridge, Mass., United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Subject Category
Navigation
Accession Number
72A17944
Distribution Limits
Public
Copyright
Other

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