ANALYSIS OF MECHANICAL SERVO DRIVE CONCEPT APPLIED TO FLIGHT CONTROLS
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 29, 1962
- Accession Number
- AD0294106