Accession Number : AD0829634

Title :   CONTROL MANEUVERS COMPONENT CHECKOUT DESCRIPTION AND PLAN, MODEL XSM-65B,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Hawk, D. N.

Report Date : 17 MAR 1958

Pagination or Media Count : 21

Abstract : This document outlines the Autopilot Gyro Package component level tests and the capability of the Control Maneuvers Checkout Equipment to perform these tests. All tests are performed with the A/P Gyro Package mounted on the test table and all cables connected in accordance with Checkout Procedure instructions. A brief description of the Autopilot Gyro Package, the Control Maneuvers Checkout Equipment, the parameters to be measured, and the method of parameter measurement is included in this document. (Author)

Descriptors :   *AUTOMATIC PILOTS), (*SURFACE TO SURFACE MISSILES, CHECKOUT PROCEDURES, GYRO STABILIZERS, ACCEPTABILITY, TEST METHODS, SEQUENCES(MATHEMATICS), ATTITUDE CONTROL SYSTEMS, GUIDED MISSILE COMPUTERS, PITCH(MOTION), ROLL, YAW, HYDRAULIC SERVOMECHANISMS, MONITORS, CHECKOUT EQUIPMENT.

Subject Categories : Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE