Add to ORKGTo assess the feasibility of a digital fly by wire system, the mechanical flight control system of an F-8C airplane was replaced with a digital primary system and an analog backup system. The Apollo computer was used as the heart of the primary system. This paper discusses the experience gained during the design and development of the system and relates it to active control systems that are anticipated for future civil transport applications
Flight control actuators and feedback sensors suitable for use in a redundant digital flight control...
A triplex digital flight control system was installed in a NASA F-8C airplane to provide fail operat...
The design, implementation, and verification of the flight control software used in the F-8 DFBW pro...
To assess the feasibility of a digital fly-by-wire system, the mechanical flight control system of a...
The feasibility of using digital fly-by-wire systems to control aircraft was demonstrated by develop...
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discuss...
Flight test results of the F-8 digital fly-by-wire (DFBW) control system are presented and the impli...
Flight test results of the F-8 digital fly by wire control system are presented and the implications...
A triplex digital fly by wire flight control system was developed and installed in an F-8C aircraft ...
The design of a fly-by-wire control system having a mission failure probability of less than one mil...
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 results of studies which were undertaken to contribute to the design of digital flight control s...
A redundant three axis analog control system was designed and developed to back up a digital fly by ...
A redundant three-axis analog control system was designed and developed to back up a digital fly-by-...
Flight control actuators and feedback sensors suitable for use in a redundant digital flight control...
A triplex digital flight control system was installed in a NASA F-8C airplane to provide fail operat...
The design, implementation, and verification of the flight control software used in the F-8 DFBW pro...
To assess the feasibility of a digital fly-by-wire system, the mechanical flight control system of a...
The feasibility of using digital fly-by-wire systems to control aircraft was demonstrated by develop...
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discuss...
Flight test results of the F-8 digital fly-by-wire (DFBW) control system are presented and the impli...
Flight test results of the F-8 digital fly by wire control system are presented and the implications...
A triplex digital fly by wire flight control system was developed and installed in an F-8C aircraft ...
The design of a fly-by-wire control system having a mission failure probability of less than one mil...
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 results of studies which were undertaken to contribute to the design of digital flight control s...
A redundant three axis analog control system was designed and developed to back up a digital fly by ...
A redundant three-axis analog control system was designed and developed to back up a digital fly-by-...
Flight control actuators and feedback sensors suitable for use in a redundant digital flight control...
A triplex digital flight control system was installed in a NASA F-8C airplane to provide fail operat...
The design, implementation, and verification of the flight control software used in the F-8 DFBW pro...