Flight Test Report of AN/ASN-82 Inertial Navigation System,

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Abstract:

A lightweight, low-cost R and D aircraft inertial navigation system is evaluated for use in Army aircraft. A brief description of the system is followed by a summary of the methods of laboratory, truck, and flight testing employed. Test results are presented and show that the system meets the design goals of 2 to 4 nautical mileshour. Problem areas uncovered during the tests are discussed in detail and areas of suggested future effort are outlined. Author

Author(s):
Clark, Raymond
Author Organization(s):
ARMY ELECTRONICS COMMAND FORT MONMOUTH NJ
Pagination:
0105

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
ECOM-3268
Task Number(s):
1H162202A21901
Project Number(s):
DA-1-H-162202-A-219
 Subject Terms
Communities of Interest:
Air Platforms
Descriptor(s):
*INERTIAL NAVIGATION, FLIGHT TESTING, STABILIZED PLATFORMS, GYRO COMPASSES, NAVIGATION COMPUTERS, DIGITAL DIFFERENTIAL ANALYZERS, MAINTAINABILITY, TEST METHODS, RELIABILITY(ELECTRONICS), POWER SUPPLIES
Field(s)/Group(s):
Air Navigation and Guidance
Keyword(s):
AN ASN 82, FLIGHT REFERENCE STABILIZATION SYSTEMS, FRSS(FLIGHT REFERENCE STABILIZATION SYSTEMS)
Report Date:
1970 Mar 01