典型的教练机训练效能计算模型对飞机的航空电子系统、操纵系统考虑不足，对飞行参数选择有局限性。
The typical computation model of training effectiveness of training plane has limitation in selection of flight parameters as well as insufficient attention to avionics and control system.
线缆耦合是HEMP对电子系统作用的主要途径之一。传输线模型是分析场线耦合常用的研究方法。
Aerial lines or cables, as one mainly energy transport path of electronic system when illuminated by HEMP, has been often modeled by field-to-transmission line model.
对于一维电子系统来说费米液体理论也不是一个好的模型，因为当应用多体微扰讨论时有红外发散，使这种最常用的方法失效了。
But it's not a much appropriate model on one-dimensional systems because of infrared divergences when many-body pertebation theory is used, thus this normal solution failed.
同时，该模型可望为复杂电磁环境下电子系统的仿生防护研究提供一定的理论和实验参考。
Meanwhile, this model can provide certain theoretical and experimental references for the bionic protection of electronic system under the complex electromagnetic environment.
本文在虚拟光学数据加密理论模型的基础上，研究一种并行电子系统实现方法。
In this article, we investigate an implementation scheme of virtual-optics based data encryption system.
本文用模糊综合评判方法与贝叶斯理论相结合，给出由小样本实验数据来确定电子系统长储可靠性模型的方法。
In this paper, a method based on the fuzzy judgement and Bayesian theory to evaluate the model of storage reliability of radio fuse using simple sample data is presented.
基于单电子系统半经典模型，分析了电阻耦合单电子晶体管的电学特性，得到其电学性能不随背景电荷分布变化的特点。
According to the semi classical model, by means of electrical characteristics analysis of R SET, it was proposed that the electrical performance of R SET was not affected by the background charge.
电子封装作为电子系统的最小组成部分，其简化模型的优劣直接影响电子系统热分析的速度和准确性。本文主要讨论单芯片封装稳态简化热模型的建立。
IC package is the smallest unit in electronic systems, compact thermal models of IC packages influence the speed and accuracy of thermal analysis directly.
根据单电子系统半经典模型，采用蒙特卡罗法单电子模拟程序对电容耦合的类CMOS单电子逻辑单元在不同参数条件下的转移特性进行数值模拟。
According to the semi classical model, the transfer characteristics of CMOS type single electron digital logic cells were analyzed by the Monte Carlo simulation.
对于采用FC（光纤通道）网络的航空电子系统，从FC的基本模型出发，给出了三种具有容错能力的常用拓扑结构：双环结构、双交换机结构和交换机仲裁环组合结构。
To the avionics of fibre channel(FC) interconnection, based on the basic FC interconnection model, three fault tolerance topologies are given: loop-to-loop, switch-to-switch and switch-loop.
对于采用FC（光纤通道）网络的航空电子系统，从FC的基本模型出发，给出了三种具有容错能力的常用拓扑结构：双环结构、双交换机结构和交换机仲裁环组合结构。
To the avionics of fibre channel(FC) interconnection, based on the basic FC interconnection model, three fault tolerance topologies are given: loop-to-loop, switch-to-switch and switch-loop.
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