Accession Number : AD0403980

Title :   PROCEEDINGS OF THE AFMDC INERTIAL GUIDANCE TEST SYMPOSIUM. VOLUME I, 16-17 OCTOBER 1962.

Corporate Author : AIR FORCE MISSILE DEVELOPMENT CENTER HOLLOMAN AFB N MEX

Report Date : 1963

Pagination or Media Count : 1

Abstract : Contents: Precision Measurement of Accelerometer Higher Order Non-linearities; Simplification of Inertial Component Test Equipment; Central Inertial Guid ance Test Facility Laboratory Standardization Efforts; Accelerometer Error Coefficients Derived From Track Tests; Testing of Stellar Inertial Guidance Systems; A Long Hard Look at Guidance System Testing; Band Concept Versus Statistical Method in Guidance Testing; The Space-Time Meas uring System of the Holloman Track; Versatile Automatic Test Equipment For Inertial Guidance Systems; Guidance System Evaluation Using The Guidance Evaluation Missile; Inertial Guidance Equipment Testing on the MIT Centrifuge.

Descriptors :   *INERTIAL GUIDANCE, *SYMPOSIA, GYROSCOPES, ACCELEROMETERS, STANDARDS, ERROR, TRACKING, TESTS METHODS, STATISTICAL PROCESSES, TIME SIGNALS, AUTOMATIC, TEST EQUIPMENT, GUIDED MISSILES, ROCKET-PROPELLED SLEDS, CENTRIFUGAL FIELDS, CENTRIFUGES, DATA PROCESS, GUIDED MISSILE COMPUTERS, RELIA, NONDESTRUCTIVE TESTING, INSTRUMENTA, CALIBRATION, SERVOMECHANISMS, CELESTIAL, TIMING CIRCUITS, TEST FACILITIES.

Distribution Statement : APPROVED FOR PUBLIC RELEASE