ABSTRACT: This paper describes development of a radiation tolerant, low power, reconfigurable avionics module aimed at meeting the avionics needs of the JPL Micro-Inspector spacecraft. This module represents a complete avionics system, consisting of two PowerPC 405 CPUs embedded within a reconfigurable FPGA fabric of over 8 Million logic gates, 64MB of EDAC protected Flash storage and 128MB of EDAC protected DDR SDRAM or SDRAM memories, along with FPGA SEU mitigation logic, and all necessary power conversion. Processor SEU mitigation is achieved by running the two processors in a lock-step and compare configuration. All of these building blocks are integrated into a double sided circuit board that takes as little as 6 square inches of board...
This paper describes high reliability radiation hardened computers built by Sandia for application a...
Abstract—This paper describes the development of a complementary GaAs PowerPC TM microprocessor suit...
This paper presents hardware and software design of the payload for the PilsenCube picosatellite. Th...
JPL has completed design of a small (\u3c 5 kg) spacecraft capable of visual inspection of a host ve...
Abstract – Future small and micro-missions, such as Mars Scouts and Deep Space probes, require a new...
NASA-JSC required an avionics platform capable of serving a wide range of applications in a cost-eff...
The need to significantly reduce the mass, power, and volume of future scientific spacecraft has res...
The performance, in-system reprogrammability, flexibility, and reduced costs of SRAM-based FPGAs mak...
This paper describes the development of a SmallSat computer system that provides increased tolerance...
Radiation hardening for coping with cosmic-ray-induced faults in electronic equipment has always bee...
This paper presents a new concept of building a high performance, radiation hardened computer from C...
Sterpone L, Porrmann M, Hagemeyer J. A Novel Fault Tolerant and Runtime Reconfigurable Platform for ...
Radiation effects on space computers are becoming more of a concern as feature sizes of modern trans...
Aim of this work is the description of a test equipment, designed to be integrated on board of a mic...
This paper summarizes the work at Lawrence Livermore National Laboratory in the development, integra...
This paper describes high reliability radiation hardened computers built by Sandia for application a...
Abstract—This paper describes the development of a complementary GaAs PowerPC TM microprocessor suit...
This paper presents hardware and software design of the payload for the PilsenCube picosatellite. Th...
JPL has completed design of a small (\u3c 5 kg) spacecraft capable of visual inspection of a host ve...
Abstract – Future small and micro-missions, such as Mars Scouts and Deep Space probes, require a new...
NASA-JSC required an avionics platform capable of serving a wide range of applications in a cost-eff...
The need to significantly reduce the mass, power, and volume of future scientific spacecraft has res...
The performance, in-system reprogrammability, flexibility, and reduced costs of SRAM-based FPGAs mak...
This paper describes the development of a SmallSat computer system that provides increased tolerance...
Radiation hardening for coping with cosmic-ray-induced faults in electronic equipment has always bee...
This paper presents a new concept of building a high performance, radiation hardened computer from C...
Sterpone L, Porrmann M, Hagemeyer J. A Novel Fault Tolerant and Runtime Reconfigurable Platform for ...
Radiation effects on space computers are becoming more of a concern as feature sizes of modern trans...
Aim of this work is the description of a test equipment, designed to be integrated on board of a mic...
This paper summarizes the work at Lawrence Livermore National Laboratory in the development, integra...
This paper describes high reliability radiation hardened computers built by Sandia for application a...
Abstract—This paper describes the development of a complementary GaAs PowerPC TM microprocessor suit...
This paper presents hardware and software design of the payload for the PilsenCube picosatellite. Th...