The validation process comprises the activities required to insure the agreement of system realization with system specification. A preliminary validation methodology for fault tolerant systems documented. A general framework for a validation methodology is presented along with a set of specific tasks intended for the validation of two specimen system, SIFT and FTMP. Two major areas of research are identified. First, are those activities required to support the ongoing development of the validation process itself, and second, are those activities required to support the design, development, and understanding of fault tolerant systems
The need for fault tolerance in Large Space systems is discussed. The unique characteristics of LSS ...
Model checking is shown to be an effective tool in validating the behavior of a fault tolerant embed...
SIFT (Software Implemented Fault Tolerance) is an experimental, fault-tolerant computer system desig...
The proceedings of the first working group meeting on validation methods for fault tolerant computer...
A computer aided reliability estimation procedure (CARE 3), developed to model the behavior of ultra...
The state of the art in the production of crucial software for flight control applications was addre...
Requirements and specifications for a method of optimizing the design of fault-tolerant flight contr...
Experiments that can be used to validate fault free performance of multiprocessor systems in aerospa...
A computer program to aid in accessing the reliability of fault tolerant avionics systems was develo...
A validation methodology for testing the performance of fault-tolerant computer systems was develope...
The requirements for fault-tolerant computers for flight control of commercial aircraft are examined...
A number of methodologies for verifying systems and computer based tools that assist users in verify...
A validation method for the synchronization subsystem of a fault tolerant computer system is investi...
Earlier generation avionics, federated architecture (FA) is used where each function has its own ind...
Literature on the specification, design, verification, testing, and evaluation of avionics systems w...
The need for fault tolerance in Large Space systems is discussed. The unique characteristics of LSS ...
Model checking is shown to be an effective tool in validating the behavior of a fault tolerant embed...
SIFT (Software Implemented Fault Tolerance) is an experimental, fault-tolerant computer system desig...
The proceedings of the first working group meeting on validation methods for fault tolerant computer...
A computer aided reliability estimation procedure (CARE 3), developed to model the behavior of ultra...
The state of the art in the production of crucial software for flight control applications was addre...
Requirements and specifications for a method of optimizing the design of fault-tolerant flight contr...
Experiments that can be used to validate fault free performance of multiprocessor systems in aerospa...
A computer program to aid in accessing the reliability of fault tolerant avionics systems was develo...
A validation methodology for testing the performance of fault-tolerant computer systems was develope...
The requirements for fault-tolerant computers for flight control of commercial aircraft are examined...
A number of methodologies for verifying systems and computer based tools that assist users in verify...
A validation method for the synchronization subsystem of a fault tolerant computer system is investi...
Earlier generation avionics, federated architecture (FA) is used where each function has its own ind...
Literature on the specification, design, verification, testing, and evaluation of avionics systems w...
The need for fault tolerance in Large Space systems is discussed. The unique characteristics of LSS ...
Model checking is shown to be an effective tool in validating the behavior of a fault tolerant embed...
SIFT (Software Implemented Fault Tolerance) is an experimental, fault-tolerant computer system desig...