Add to ORKGThe purpose of this test was to evaluate the Digital Flight Control System (DFOS), Operational Flight Program (OFP) 4.2.2 as installed in the F-14A Tomcat for the all-weather aircraft earner landing mission
Despite the recent improvements to the T-38 airframe and engines, the United States Air Force is sti...
Delivering communications from high altitudes, at airspeeds of just 30 knots, gathering data from ac...
The purpose of this thesis is to document the handling qualities of the V-22 tiltrotor aircraft in i...
A flight test evaluation of the digital elctronic engine control (DEEC) system was conducted. An ove...
The E-2C aircraft is a Navy carrier based high-wing, twin engine turboprop powered aircraft used for...
This thesis analyzes the recent Version 10.7 Operational Flight Program (v10.7 OFP) Flight Control S...
The third phase of a flight evaluation of a digital electronic engine control system in an F-15 has ...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...
Flight test results of the F-8 digital fly-by-wire (DFBW) control system are presented and the impli...
The MV-22 Osprey tiltrotor aircraft is a radically new air vehicle designed to replace aging helic...
The Precision Approach and Landing System (PALS) is an Electronic Landing Aid (ELA) installed aboard...
The purpose of this thesis was to flight test the University of Tennessee Space Institute’s PA-32 Sa...
The Rotary Wing Ship Suitability Branch of the Naval Air Warfare Center Aircraft Division, Patuxent ...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
A study to assess the utility of an aircraft referenced 3D audio display was undertaken to determine...
Despite the recent improvements to the T-38 airframe and engines, the United States Air Force is sti...
Delivering communications from high altitudes, at airspeeds of just 30 knots, gathering data from ac...
The purpose of this thesis is to document the handling qualities of the V-22 tiltrotor aircraft in i...
A flight test evaluation of the digital elctronic engine control (DEEC) system was conducted. An ove...
The E-2C aircraft is a Navy carrier based high-wing, twin engine turboprop powered aircraft used for...
This thesis analyzes the recent Version 10.7 Operational Flight Program (v10.7 OFP) Flight Control S...
The third phase of a flight evaluation of a digital electronic engine control system in an F-15 has ...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...
Flight test results of the F-8 digital fly-by-wire (DFBW) control system are presented and the impli...
The MV-22 Osprey tiltrotor aircraft is a radically new air vehicle designed to replace aging helic...
The Precision Approach and Landing System (PALS) is an Electronic Landing Aid (ELA) installed aboard...
The purpose of this thesis was to flight test the University of Tennessee Space Institute’s PA-32 Sa...
The Rotary Wing Ship Suitability Branch of the Naval Air Warfare Center Aircraft Division, Patuxent ...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
A study to assess the utility of an aircraft referenced 3D audio display was undertaken to determine...
Despite the recent improvements to the T-38 airframe and engines, the United States Air Force is sti...
Delivering communications from high altitudes, at airspeeds of just 30 knots, gathering data from ac...
The purpose of this thesis is to document the handling qualities of the V-22 tiltrotor aircraft in i...