HELICOPTER TESTING OF INERTIAL NAVIGATION SYSTEMS

VFS-F28-020

5/17/1972

Authors
Abstract
Content

During the last decade, inertial navigation systems have undergone two generations of improvement, They have become lighter, less costly, and consequently have become more attractive for various helicopter applications. During this period, a number of flight test programs have been conducted on this equipment, beginning with the Navy-sponsored flight test of a Litton LN-3 in an HUS-1 in 1962 and culminating with the recently completed flight testing of the Litton AN/ASN-109 at Holloman AFB. The results of these programs are presented here.

Meta TagsDetails
DOI
https://doi.org/10.4050/VFS-F28-020
Citation
Hughes, J., "HELICOPTER TESTING OF INERTIAL NAVIGATION SYSTEMS," Forum 28 - Washington, D.C. 1972, Washington, D.C., May 17, 1972, https://doi.org/10.4050/VFS-F28-020.
Additional Details
Publisher
Published
5/17/1972
Product Code
VFS-F28-020
Content Type
Technical Paper
Language
English