Add to ORKGOperating procedures for this redundant system are described. A test plan is developed with two obje...
An analysis of the effects of discrete failures on the data processing subsystem is presented. A fun...
Criteria and concepts for onboard checkout and monitoring system for space shuttle propulsion system...
A failure detection and isolation philosophy applicable to multiple off-the-shelf gimbaled IMUs are ...
STAR computer has five redundant modular function units, fixed store, arithmetic, memory, input, and...
The background of the shuttle avionics system design and the unique drivers associated with the redu...
Means for evaluating data bus architectures and protocols for highly integrated flight control syste...
The computer subsystem of the Villanova University GAS (Get Away Special) experiment apparatus is di...
The reliability of electronic systems is a significant challenge in the development of new devices.I...
Development of onboard checkout equipment and performance monitoring capability for space shuttles -...
The software for selected space shuttle components are examined for potential problem areas and poss...
The shuttle system of interest in this paper is the shuttle's data processing system (DPS). The DPS ...
The SpaceHab 1 flight on STS-57 served as a test platform for evaluation of two space station payloa...
Candidate designs and their software implementation are presented for the Orbital Maneuvering System...
The challenge of providing redundancy management (RM) and fault tolerance to meet the Shuttle Progra...
Operating procedures for this redundant system are described. A test plan is developed with two obje...
An analysis of the effects of discrete failures on the data processing subsystem is presented. A fun...
Criteria and concepts for onboard checkout and monitoring system for space shuttle propulsion system...
A failure detection and isolation philosophy applicable to multiple off-the-shelf gimbaled IMUs are ...
STAR computer has five redundant modular function units, fixed store, arithmetic, memory, input, and...
The background of the shuttle avionics system design and the unique drivers associated with the redu...
Means for evaluating data bus architectures and protocols for highly integrated flight control syste...
The computer subsystem of the Villanova University GAS (Get Away Special) experiment apparatus is di...
The reliability of electronic systems is a significant challenge in the development of new devices.I...
Development of onboard checkout equipment and performance monitoring capability for space shuttles -...
The software for selected space shuttle components are examined for potential problem areas and poss...
The shuttle system of interest in this paper is the shuttle's data processing system (DPS). The DPS ...
The SpaceHab 1 flight on STS-57 served as a test platform for evaluation of two space station payloa...
Candidate designs and their software implementation are presented for the Orbital Maneuvering System...
The challenge of providing redundancy management (RM) and fault tolerance to meet the Shuttle Progra...
Operating procedures for this redundant system are described. A test plan is developed with two obje...
An analysis of the effects of discrete failures on the data processing subsystem is presented. A fun...
Criteria and concepts for onboard checkout and monitoring system for space shuttle propulsion system...