The modeling and analysis of transient faults in microprocessor based controllers are discussed. Such controllers typically consist of a microprocessor, read only memory storing and application program, random access memory for data storage, and input/output devices for external communications. The effects of transient faults on the performance of the controller are reviewed. An instruction level perspective of performance is taken which is the basis of a useful high level program state description of the microprocessor controller. A transition matrix is defined which determines the controller's response to transient fault arrivals
An electronic computing device including at least one processing unit that implements a specific fau...
The support software package is described which exists for the advanced on-board processor (AOP) bei...
The objective of the Multi-Path Redundant Avionics Suite (MPRAS) program is the development of a set...
This report describes the use of the V/STOL Aircraft Sizing and Performance Computer Program (VASCOM...
Containment set techniques are applied to 8085 microprocessor controllers so as to transform a typic...
The computer program written in support of the problem to determine aerodynamic influence coefficien...
Operating instructions, design requirement, and description of Air Bearing Platform, T50-
A computer program is described for calculating the flexibility coefficients as arm design changes a...
This internship provided an opportunity for an intern to work with NASA's Ground Support Equipment (...
The Federal Aviation Administration (FAA) and NASA conducted a full-scale air-to-surface impact-surv...
Computer program documentation and user manual for steady state attitude control propulsion system -...
An apparatus is provided that includes a plurality of modules, a plurality of memory banks, and a mu...
All 34 malfunction symptoms and 2 Special subroutines associated with the five subsystems operating ...
Critical information required for the design of integrated avionics suitable for generation aviation...
The researchers at the Langley Research Center Flight Simulation Computing System are provided with ...
An electronic computing device including at least one processing unit that implements a specific fau...
The support software package is described which exists for the advanced on-board processor (AOP) bei...
The objective of the Multi-Path Redundant Avionics Suite (MPRAS) program is the development of a set...
This report describes the use of the V/STOL Aircraft Sizing and Performance Computer Program (VASCOM...
Containment set techniques are applied to 8085 microprocessor controllers so as to transform a typic...
The computer program written in support of the problem to determine aerodynamic influence coefficien...
Operating instructions, design requirement, and description of Air Bearing Platform, T50-
A computer program is described for calculating the flexibility coefficients as arm design changes a...
This internship provided an opportunity for an intern to work with NASA's Ground Support Equipment (...
The Federal Aviation Administration (FAA) and NASA conducted a full-scale air-to-surface impact-surv...
Computer program documentation and user manual for steady state attitude control propulsion system -...
An apparatus is provided that includes a plurality of modules, a plurality of memory banks, and a mu...
All 34 malfunction symptoms and 2 Special subroutines associated with the five subsystems operating ...
Critical information required for the design of integrated avionics suitable for generation aviation...
The researchers at the Langley Research Center Flight Simulation Computing System are provided with ...
An electronic computing device including at least one processing unit that implements a specific fau...
The support software package is described which exists for the advanced on-board processor (AOP) bei...
The objective of the Multi-Path Redundant Avionics Suite (MPRAS) program is the development of a set...