The Radiation Tolerant, FPGA-based SmallSat Computer System (RadSat) computing platform exploits a commercial off-the-shelf (COTS) Field Programmable Gate Array (FPGA) with real-time partial reconfiguration to provide increased performance, power efficiency and radiation tolerance at a fraction of the cost of existing radiation hardened computing solutions. This technology is ideal for small spacecraft that require state-of-the-art on-board processing in harsh radiation environments but where using radiation hardened processors is cost prohibitive
Field programmable gate arrays (FPGA) are used in every space application. Currently, most space fli...
Miniaturized satellites enable a variety space missions which were in the past infeasible, impractic...
Today, with the rise of the private sector in space exploration, space missions are becoming more fr...
This paper describes the development of a SmallSat computer system that provides increased tolerance...
Radiation effects on space computers are becoming more of a concern as feature sizes of modern trans...
In today's rapidly advancing technology roadmap for space applications there is an emphasis on compl...
In today's budgetary environment, there is significant interest within the National Aeronautics and ...
CubeSats are small satellites used for scientific experiments because they cost less than full sized...
Sterpone L, Porrmann M, Hagemeyer J. A Novel Fault Tolerant and Runtime Reconfigurable Platform for ...
In this contribution, we present a CubeSat-compatible on-board computer (OBC) architecture that offe...
CubeSat missions needs components that are tolerant against the radiation in space. The hardware com...
The Goddard Modular Smallsat Architecture (GMSA) is developed at NASA Goddard Space Flight Center (G...
The performance, in-system reprogrammability, flexibility, and reduced costs of SRAM-based FPGAs mak...
FPGA use in space-based applications is becoming more common. Radiation-hardened (rad-hard) memories...
The purpose of this thesis is to design and test a fault–tolerant reduced instruction set computer p...
Field programmable gate arrays (FPGA) are used in every space application. Currently, most space fli...
Miniaturized satellites enable a variety space missions which were in the past infeasible, impractic...
Today, with the rise of the private sector in space exploration, space missions are becoming more fr...
This paper describes the development of a SmallSat computer system that provides increased tolerance...
Radiation effects on space computers are becoming more of a concern as feature sizes of modern trans...
In today's rapidly advancing technology roadmap for space applications there is an emphasis on compl...
In today's budgetary environment, there is significant interest within the National Aeronautics and ...
CubeSats are small satellites used for scientific experiments because they cost less than full sized...
Sterpone L, Porrmann M, Hagemeyer J. A Novel Fault Tolerant and Runtime Reconfigurable Platform for ...
In this contribution, we present a CubeSat-compatible on-board computer (OBC) architecture that offe...
CubeSat missions needs components that are tolerant against the radiation in space. The hardware com...
The Goddard Modular Smallsat Architecture (GMSA) is developed at NASA Goddard Space Flight Center (G...
The performance, in-system reprogrammability, flexibility, and reduced costs of SRAM-based FPGAs mak...
FPGA use in space-based applications is becoming more common. Radiation-hardened (rad-hard) memories...
The purpose of this thesis is to design and test a fault–tolerant reduced instruction set computer p...
Field programmable gate arrays (FPGA) are used in every space application. Currently, most space fli...
Miniaturized satellites enable a variety space missions which were in the past infeasible, impractic...
Today, with the rise of the private sector in space exploration, space missions are becoming more fr...