TY - JOUR
T1 - Design of double-upset recoverable and transient-pulse filterable latches for low-power and low-orbit aerospace applications
AU - Yan, Aibin
AU - Chen, Yan
AU - Xu, Zhelong
AU - Chen, Zhili
AU - Cui, Jie
AU - Huang, Zhengfeng
AU - Girard, Patrick
AU - Wen, Xiaoqing
N1 - Publisher Copyright:
© 2018 EDP Sciences. All rights reserved.
PY - 2020/10
Y1 - 2020/10
N2 - To meet the requirements of both high reliability and low power in low-orbit aerospace applications, this article first presents a singleevent Double-Upset (SEDU) self-Recoverable and single-event Transient (SET) Pulse Filterable (DURTPF) latch design with low power. The DURTPF latch mainly consists of eight mutually feeding-back C-elements (CEs) and an SET pulse filterable Schmitt-trigger (ST). To make an ST behave not only as a pulse filterable ST but also as an error interceptive CE, an input-split ST is created, leading to an enhancedversion of theDURTPF latch, namelyDURTPF-EV.TheDURTPF-EV latch mainly consists of seven mutually feeding-back CEs including an input-split ST. Simulation results demonstrate both the SEDU self-recoverability and SET pulse filterability of the proposed latches at the cost ofmoderate silicon area. Using the clock gating technology, the DURTPF latch reduces power dissipation by about 63% on average compared with the state-of-the-art SEDU self-recoverable latch designs that are not SET-pulse filterable. Moreover, the DURTPF-EV latch is more cost-effective and its reliability is also enhanced, making it more suitable for low power and low-orbit aerospace applications.
AB - To meet the requirements of both high reliability and low power in low-orbit aerospace applications, this article first presents a singleevent Double-Upset (SEDU) self-Recoverable and single-event Transient (SET) Pulse Filterable (DURTPF) latch design with low power. The DURTPF latch mainly consists of eight mutually feeding-back C-elements (CEs) and an SET pulse filterable Schmitt-trigger (ST). To make an ST behave not only as a pulse filterable ST but also as an error interceptive CE, an input-split ST is created, leading to an enhancedversion of theDURTPF latch, namelyDURTPF-EV.TheDURTPF-EV latch mainly consists of seven mutually feeding-back CEs including an input-split ST. Simulation results demonstrate both the SEDU self-recoverability and SET pulse filterability of the proposed latches at the cost ofmoderate silicon area. Using the clock gating technology, the DURTPF latch reduces power dissipation by about 63% on average compared with the state-of-the-art SEDU self-recoverable latch designs that are not SET-pulse filterable. Moreover, the DURTPF-EV latch is more cost-effective and its reliability is also enhanced, making it more suitable for low power and low-orbit aerospace applications.
UR - https://www.scopus.com/pages/publications/85105864697
U2 - 10.1109/TAES.2020.2982341
DO - 10.1109/TAES.2020.2982341
M3 - 文章
AN - SCOPUS:85105864697
SN - 0018-9251
VL - 56
SP - 3931
EP - 3940
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 5
ER -