Flight test results of the F-8 digital fly by wire control system are presented and the implications for application to active control technology are discussed. The F-8 DFBW system has several of the attributes of proposed ACT systems, so the flight test experience is helpful in assessing the capabilities of those systems. Topics of discussion include the predicted and actual flight performance of the control system, assessments of aircraft flying qualities and other piloting factors, software management and control, and operational experience
A summary of the YF-16 flight control system is presented. The basic functions of the flight control...
The advanced fighter technology integration (AFTI) F-16 aircraft is a highly complex digital flight ...
Five flight tests of the Digital Automated Landing System (DIALS) were conducted on the Advanced Tra...
Flight test results of the F-8 digital fly-by-wire (DFBW) control system are presented and the impli...
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discuss...
To assess the feasibility of a digital fly by wire system, the mechanical flight control system of a...
To assess the feasibility of a digital fly-by-wire system, the mechanical flight control system of a...
A triplex digital fly by wire flight control system was developed and installed in an F-8C aircraft ...
The feasibility of using digital fly-by-wire systems to control aircraft was demonstrated by develop...
The handling qualities of the F-8 digital fly-by-wire airplane are evaluated by using the Cooper-Har...
The handling qualities of the F-8 digital fly by wire airplane are evaluated by using the Cooper-Har...
The design, implementation, and verification of the flight control software used in the F-8 DFBW pro...
The design, implementation, and verification of the flight control software used in the F-8 DFBW pro...
The design of a fly-by-wire control system having a mission failure probability of less than one mil...
A triplex digital flight control system was installed in a NASA F-8C airplane to provide fail operat...
A summary of the YF-16 flight control system is presented. The basic functions of the flight control...
The advanced fighter technology integration (AFTI) F-16 aircraft is a highly complex digital flight ...
Five flight tests of the Digital Automated Landing System (DIALS) were conducted on the Advanced Tra...
Flight test results of the F-8 digital fly-by-wire (DFBW) control system are presented and the impli...
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discuss...
To assess the feasibility of a digital fly by wire system, the mechanical flight control system of a...
To assess the feasibility of a digital fly-by-wire system, the mechanical flight control system of a...
A triplex digital fly by wire flight control system was developed and installed in an F-8C aircraft ...
The feasibility of using digital fly-by-wire systems to control aircraft was demonstrated by develop...
The handling qualities of the F-8 digital fly-by-wire airplane are evaluated by using the Cooper-Har...
The handling qualities of the F-8 digital fly by wire airplane are evaluated by using the Cooper-Har...
The design, implementation, and verification of the flight control software used in the F-8 DFBW pro...
The design, implementation, and verification of the flight control software used in the F-8 DFBW pro...
The design of a fly-by-wire control system having a mission failure probability of less than one mil...
A triplex digital flight control system was installed in a NASA F-8C airplane to provide fail operat...
A summary of the YF-16 flight control system is presented. The basic functions of the flight control...
The advanced fighter technology integration (AFTI) F-16 aircraft is a highly complex digital flight ...
Five flight tests of the Digital Automated Landing System (DIALS) were conducted on the Advanced Tra...