Accession Number:

AD0294106

Title:

ANALYSIS OF MECHANICAL SERVO DRIVE CONCEPT APPLIED TO FLIGHT CONTROLS

Descriptive Note:

Corporate Author:

NORTH AMERICAN AVIATION INC LOS ANGELES CALIF

Personal Author(s):

Report Date:

1962-09-29

Pagination or Media Count:

1.0

Abstract:

Investigation of an all mechanical aileron control system including a mechanical proportional toroidal servo is described. A system having specified characteristics will provide satisfactory performance and this system is deemed feasible within present state of the art component development. Analog representations AND RESULTS OF SYSTEM PARAMETER VARIATION STUDIES ARE PRESENTED. Schematics, system and servo characteristics, and pictorial reproductions are contained. Author

Descriptors:

• *AILERONS
• ANALOG COMPUTERS
• CONTROL SYSTEMS
• JET FIGHTERS
• SERVOMECHANISMS
• SIMULATION
• THEORY

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE