Accession Number : AD0829439

Title :   GUIDANCE DATA CONVERTER SYSTEM OPERATION AND LOGIC,

Corporate Author : GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Personal Author(s) : Marenholtz, P. E.

Report Date : 27 JUN 1956

Pagination or Media Count : 21

Abstract : The Guidance Data Converter is a missileborne component of the Autopilot Subsystem as configured for application to the radio inertial guidance system. This technical note covers the overall operation and system logic.

Descriptors :   (*SURFACE TO SURFACE MISSILES, NAVIGATION COMPUTERS), COMMAND GUIDANCE, INERTIAL GUIDANCE, LOGIC CIRCUITS, ACCELEROMETERS, INTEGRATORS, GUIDED MISSILE TRACKING SYSTEMS, VELOCITY, ANALOG SYSTEMS, RELAXATION OSCILLATORS.

Subject Categories : Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE