Flight Test of a G. E. and DCI Direct Drive Fly-By-Wire Flight Control System.

摘要

This report describes the flight test of two Fly-By-Wire flight control systems which use direct drive control valves. The test aircraft is an F-4E and the test systems are used to control the left aileron of the test aircraft. One test system was developed by the General Electric Company and the other by Dynamic Controls, Inc. The report describes the test systems, the aircraft installation, flight test and results. (Author)