An SET-free, fully-digital point-of-load regulator for next-generation spacecraft power systems

Nijad Anabtawi, Rabih Chamoun
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引用次数: 1

Abstract

This paper presents a digitally controlled point-of-load regulator for next-generation power systems. It is intended for spacecraft with limited energy harvesting capability and on board battery storage such as micro- and nano-satellites as well as multi-tier power distribution networks of conventional satellite and spacecraft subsystems. The novel control loop was designed to minimize radiation induced single-event effects (SEE) and resulting transients. The design was implemented in 14nm bulk complimentary metal-oxide semiconductor (CMOS) process and validated with post layout simulations. It attains a peak efficiency of 95% at heavy load conditions and 79% at light loads with a maximum voltage ripple of 25mV at light loads. The most susceptible elements of the proposed regulator have a relatively high energy threshold (~ 15pJ corresponding to 40 MeV.cm2/mg) indicating a small probability of occurrence in harsh environments and no catastrophic failure.
用于下一代航天器动力系统的无set、全数字负载点调节器
提出了一种适用于下一代电力系统的数字控制负载点调节器。它用于具有有限能量收集能力和机载电池存储的航天器,如微型和纳米卫星,以及传统卫星和航天器子系统的多层配电网络。新的控制回路被设计为最小化辐射引起的单事件效应(SEE)和由此产生的瞬态。该设计采用14nm CMOS工艺实现,并通过布局后仿真验证。它在重负载条件下达到95%的峰值效率,在轻负载条件下达到79%,轻负载时最大电压纹波为25mV。所提出的调节器的最敏感元件具有相对较高的能量阈值(~ 15pJ对应于40 MeV.cm2/mg),表明在恶劣环境中发生的概率很小,不会发生灾难性故障。
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