NASA NTRS · 19860000215
Laser Inertial Navigation System
Abstract
Acceptable 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.
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Hruby, R. J., Xenakis, G., Carestia, R. A., Bjorkman, W. S., Schmit, S. F., Corliss, L. D.. 1986-05-01. Laser Inertial Navigation System. https://ntrs.nasa.gov/citations/19860000215
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