Aircraft Hydraulic Servomechanisms.
Abstract
The authors have attempted to present to others concerned with the analysis, design, and testing of integrated aircraft control systems, certain fundamental information regarding the hydraulic servomechanisms used to position the aircraft control surfaces. This is accomplished primarily by means of developing mathematical models for the performance of hydraulic servomechanisms with both mechanical and electrical inputs.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1969
- Accession Number
- AD0859682
Entities
People
- Augustus P. Henry
- Dunstan Graham
- Gordon E. Click
- Irving L. Ashkenas
- James W. Hager