Accession Number:

AD0872255

Title:

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

Descriptive Note:

Corporate Author:

ARMY ELECTRONICS COMMAND FORT MONMOUTH NJ

Personal Author(s):

• Clark, Raymond

Report Date:

1970-03-01

Pagination or Media Count:

105.0

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

Descriptors:

• *INERTIAL NAVIGATION
• FLIGHT TESTING
• STABILIZED PLATFORMS
• GYRO COMPASSES
• NAVIGATION COMPUTERS
• DIGITAL DIFFERENTIAL ANALYZERS
• MAINTAINABILITY
• TEST METHODS
• RELIABILITY(ELECTRONICS)
• POWER SUPPLIES

Subject Categories:

• Air Navigation and Guidance

Distribution Statement:

APPROVED FOR PUBLIC RELEASE