Accession Number:

AD0829439

Title:

GUIDANCE DATA CONVERTER SYSTEM OPERATION AND LOGIC,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Personal Author(s):

• Marenholtz, P. E.

Report Date:

1956-06-27

Pagination or Media Count:

21.0

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