飞机主电源系统关键器件健康状态评估研究
李小宁, 高朝晖, 王爽, 汤孝, 李一卓
Research on Health Assessment Method of Key Components in Aircraft Main Power System
LI Xiaoning, GAO Zhaohui, WANG Shuang, TANG Xiao, LI Yizhuo
表3
蒙特卡罗仿真组中关键器件参数分布设置
仿真组
二极管正向电压
/
V
二极管反向漏电流
/
A
MOS管导通电阻
/
Ω
循环仿真次数
1
(1.8,0.1)
(25μ,0.99)
(0.6,0.5)
30
2
(1.2,0.25)
30
3
(1.8,0.17)
30
4
(2.4,0.12)
30
5
(2.4,0.1)
(75μ,0.33)
(0.6,0.5)
30
6
(1.2,0.25)
30
7
(1.8,0.17)
30
8
(2.4,0.12)
30
9
(2.9,0.08)
(125μ,0.2)
(0.6,0.5)
30
10
(1.2,0.25)
30
11
(1.8,0.17)
30
12
(2.4,0.12)
30
13
(3.4,0.06)
(175μ,0.14)
(0.6,0.5)
30
14
(1.2,0.25)
30
15
(1.8,0.17)
30
16
(2.4,0.12)
30