The requirements for fault-tolerant computers for flight control of commercial aircraft are examined; it is concluded that the reliability requirements far exceed those typically quoted for space missions. Examination of circuit technology and alternative computer architectures indicates that the desired reliability can be achieved with several different computer structures, though there are obvious advantages to those that are more economic, more reliable, and, very importantly, more certifiable as to fault tolerance. Progress in this field is expected to bring about better computer systems that are more rigorously designed and analyzed even though computational requirements are expected to increase significantly
A methodology for the design of a tightly coupled, highly reliable microprocessor based computer sys...
Emulation techniques are proposed as a solution to a difficulty arising in the analysis of the relia...
System architectures which incorporate fail operative flight guidance functions within a total integ...
This final report summarizes the work on the design of a fault tolerant digital computer for aircraf...
This volume is concerned with the architecture of a fault tolerant digital computer for an advanced ...
The reliability of adaptive controls for future aircraft are discussed. The research, formulation, a...
A highly-reliable, fault-tolerant reconfigurable computer system for aircraft applications was devel...
Concepts for software to implement real time aircraft control systems on a centralized digital compu...
Requirements and specifications for a method of optimizing the design of fault-tolerant flight contr...
A digital computer subsystem fault-tolerant concept was defined, and the potential benefits and cost...
Problems related to the design of the hardware for an integrated aircraft electronic system are cons...
The central thesis of this research is toward the concept of reliability through redundancy for comp...
A computer aided reliability estimation procedure (CARE 3), developed to model the behavior of ultra...
Bibliography and new techniques for use of error correction and redundancy to improve reliability of...
This report analyzes the reliability of NASA's Ultra-reliable Fault Tolerant Control System (UFTCS) ...
A methodology for the design of a tightly coupled, highly reliable microprocessor based computer sys...
Emulation techniques are proposed as a solution to a difficulty arising in the analysis of the relia...
System architectures which incorporate fail operative flight guidance functions within a total integ...
This final report summarizes the work on the design of a fault tolerant digital computer for aircraf...
This volume is concerned with the architecture of a fault tolerant digital computer for an advanced ...
The reliability of adaptive controls for future aircraft are discussed. The research, formulation, a...
A highly-reliable, fault-tolerant reconfigurable computer system for aircraft applications was devel...
Concepts for software to implement real time aircraft control systems on a centralized digital compu...
Requirements and specifications for a method of optimizing the design of fault-tolerant flight contr...
A digital computer subsystem fault-tolerant concept was defined, and the potential benefits and cost...
Problems related to the design of the hardware for an integrated aircraft electronic system are cons...
The central thesis of this research is toward the concept of reliability through redundancy for comp...
A computer aided reliability estimation procedure (CARE 3), developed to model the behavior of ultra...
Bibliography and new techniques for use of error correction and redundancy to improve reliability of...
This report analyzes the reliability of NASA's Ultra-reliable Fault Tolerant Control System (UFTCS) ...
A methodology for the design of a tightly coupled, highly reliable microprocessor based computer sys...
Emulation techniques are proposed as a solution to a difficulty arising in the analysis of the relia...
System architectures which incorporate fail operative flight guidance functions within a total integ...