Accession Number:

AD0829634

Title:

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

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Hawk, D. N.

Report Date:

1958-03-17

Pagination or Media Count:

21.0

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 AP 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