DocumentCode
1175257
Title
Advanced Development of ESG Strapdown Navigation Systems
Author
Christensen, T.W.
Author_Institution
Honeywell Inc. St. Petersburg, Fla.
Issue
2
fYear
1966
fDate
3/1/1966 12:00:00 AM
Firstpage
143
Lastpage
157
Abstract
The fundamental problem of inertial navigation, double integration of acceleration to obtain position, is defined and discussed. Mechanizations of both space-stable and local-vertical platform systems are exhibited. The synthesis problem for an electrically suspended gyro (ESG) strapdown system is defined and discussed: readout, readout errors due to vehicle motion, synchronization of readout with system computer, alignment, correction and calibration for mass unbalance drift, and digital mechanization. Alignment, calibration, and acceleration measurement are also discussed. Sources of error involved in the electronic gimbaling including those peculiar to strapdown configuration are discussed and compared to mechanically gimbaled systems. Advanced developments required in the component and systems areas are listed, and it is shown that such development will lead to reduced complexity, higher accuracy, and increased reliability and utility for inertial systems.
Keywords
Acceleration; Accelerometers; Assembly; Calibration; Computer errors; Gyroscopes; Inertial navigation; Maintenance; Temperature control; Vehicles; Electrostatic; gimbaling; gyroscope; inertial; navigation; strapdown; system;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1966.4501736
Filename
4501736
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