Results 171 to 180 of about 16,144 (237)
Empirical Modeling of Single-Event Upset (SEU) in NMOS Depletion-Mode-Load Static RAM (SRAM) Chips
J. A. Zoutendyk +5 more
openalex +2 more sources
Investigation of single-event upset (SEU) in an advanced bipolar process
J. A. Zoutendyk +2 more
openalex +2 more sources
Single-Event Upset (SEU) in a Dram with On-Chip Error Correction
J. A. Zoutendyk +4 more
openalex +2 more sources
Error detection and correction of single event upset (SEU) tolerant latch
Norhuzaimin Julai +2 more
openalex +2 more sources
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IEEE Transactions on Nuclear Science, 2023
Upsets due to low-energy protons are a concern for highly scaled technology nodes as critical charges for storage cells continue to decrease. This work evaluates the single-event upset (SEU) vulnerability of D-flip-flop (FF) and static random access ...
Y. Xiong +5 more
semanticscholar +1 more source
Upsets due to low-energy protons are a concern for highly scaled technology nodes as critical charges for storage cells continue to decrease. This work evaluates the single-event upset (SEU) vulnerability of D-flip-flop (FF) and static random access ...
Y. Xiong +5 more
semanticscholar +1 more source
Single-Event Upset in 3-D Charge-Trap NAND Flash Memories
IEEE Transactions on Electron Devices, 2022The effects of single-event upset (SEU) on the threshold voltage ( ${V}_{T}$ ) of a programmed cell in 3-D charge-trap (CT) NAND flash memory have been investigated using 3-D technology-computer-aided design (TCAD) simulations.
Joung-June Park +6 more
semanticscholar +1 more source
Radiation Effects Data Workshop, 2022
Proton induced SEU cross-sections of the Movidius Myriad X VPU and Google Edge TPU are presented. Upset rates in the space radiation environment are estimated and found to be acceptable for low orbit missions.
Devin P. Ramaswami +4 more
semanticscholar +1 more source
Proton induced SEU cross-sections of the Movidius Myriad X VPU and Google Edge TPU are presented. Upset rates in the space radiation environment are estimated and found to be acceptable for low orbit missions.
Devin P. Ramaswami +4 more
semanticscholar +1 more source

