DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
AD0294106
Title:
ANALYSIS OF MECHANICAL SERVO DRIVE CONCEPT APPLIED TO FLIGHT CONTROLS
Corporate Author:
NORTH AMERICAN AVIATION INC LOS ANGELES CALIF
Report Date:
1962-09-29
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
Pages:
0001
Contract Number:
NOW62 1076
File Size:
0.00MB
