EVALUATION OF A MECHANICAL FLIGHT CONTROL SERVO

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Abstract:

Continuation of the investigation of an all mechanical proportional toroidal servo including the formulation of procurement definition, design of an adaptation to an existing F100 simulator all mechanical aileron control system, and specific procurement commitment are described. Author

Author(s):
No Author(s) Identified
Author Organization(s):
NORTH AMERICAN AVIATION INC LOS ANGELES CALIF
Annotation:
F-100 AILERON FLIGHT CONTROL SYSTEM SIMULATION DESIGN AND EVALUATION.
Pagination:
0001

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Contract/Grant Number(s):
NOW62 1076
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*AILERONS, CONTROL SYSTEMS, FEEDBACK, FLIGHT INSTRUMENTS, SERVOMECHANISMS, SPECTROGRAPHIC CAMERAS
Keyword(s):
F 100 AIRCRAFT
Report Date:
1962 Nov 30