Accession Number : AD0872255

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

Corporate Author : ARMY ELECTRONICS COMMAND FORT MONMOUTH NJ

Personal Author(s) : Clark, Raymond

Report Date : MAR 1970

Pagination or Media Count : 105

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 miles/hour. 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