ANALYSIS OF THE ROSS CONTROL SYSTEM INSTALLED IN A T-33 AIRCRAFT,
Abstract
An analysis is made of the Ross rudder-aileron interconnect system through partial use of servo analysis techniques, as well as discuss some other aspects of the system. The Ross Control System is a two part mechanical device which combines the action of the aileron and rudder of an aircraft in an attempt to produce coorinated flight on one hand and cross controlled flight on the other. The first is a double differential unit which varies the ratio of rudder deflection to aileron deflection, depending upon the position of the elevator. The second is an adjustor unit which permits variance of the rudder-aileron ratio range. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1962
- Accession Number
- AD0422246
Entities
People
- Arthur G. Jones