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Laser Inertial Navigation SystemAcceptable accuracy obtained with short alignment time. Report describes successful helicopter tests of laser inertial navigational equipment. Tests conducted over 3-year period, both in laboratory and flight. Inertial system used as position/velocity/attitude indicator and later also served as part of automatic flight-control system.
Document ID
19860000215
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Hruby, R. J. (University of Southern Colorado)
Xenakis, G. (Analytical Mechanics Associates, Inc.)
Carestia, R. A. (Analytical Mechanics Associates, Inc.)
Bjorkman, W. S. (U.S. Army Aeromechanics Laboratory)
Schmit, S. F.
Corliss, L. D.
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 10
Issue: 3
ISSN: 0145-319X
Subject Category
Electronic Systems
Report/Patent Number
ARC-11473
Accession Number
86B10215
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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