Hostname: page-component-cd9895bd7-7cvxr Total loading time: 0 Render date: 2024-12-18T04:54:49.244Z Has data issue: false hasContentIssue false

Strapped Down Inertial Navigation Systems

Published online by Cambridge University Press:  18 January 2010

R. P. G. Collinson
Affiliation:
(Marconi-Elliott Avionics Systems, Ltd.)

Extract

The heart of an inertial navigation system is the Inertial Measuring Unit (I.M.U.) as this carries out the fundamental tasks of measuring the vehicle acceleration and providing a spatial reference. The I.M.U. thus determines the system performance and accuracy; it also accounts for about two thirds of the initial cost of the system and is a major factor in the cost of ownership.

Up to now the majority of IN systems have used a stable platform I.M.U. where the gyros and accelerometers are mounted on a gimbal suspended platform which is servo controlled from the gyros. This has greatly eased the task of developing suitable gyros of the required accuracy, as the gimbal stabilization system isolates the gyros from the angular motion of the vehicle and greatly simplifies the subsequent computation in terms of axis transformations; it provides a direct read out of the euler angles—heading, pitch and roll. However such a system is inevitably mechanically complex and its ultimate reliability is constrained by such components as slip rings, servo motors, synchros, resolvers, encoders, gimbal bearings &c.

Type
Research Article
Copyright
Copyright © The Royal Institute of Navigation 1973

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCE

1Sapuppo, M. S. and Pijoan, P. J. (1970). A small low angular momentum inertial gyroscope, A.I.A.A. paper 70—1011, Massachusetts Institute of Technology, Draper Laboratory, Cambridge, Mass., U.S.A.Google Scholar