Ultra-low risk assessment under the confirmed compliance of automatic aircraft landing characteristics with airworthiness requirements
- 作者: Aleksandrovskaya L.1, Ardalionova A.2, Kirillin A.1
-
隶属关系:
- Moscow State Aviation Technological University (MATI)
- Moscow Institute of Electromechanics and Automatics (MIEA)
- 期: 卷 55, 编号 2 (2016)
- 页面: 232-241
- 栏目: Systems Analysis and Operations Research
- URL: https://journals.rcsi.science/1064-2307/article/view/219583
- DOI: https://doi.org/10.1134/S1064230716010032
- ID: 219583
如何引用文章
详细
Two techniques for approximating the tails of the probability distribution of automatic aircraft landing characteristics are considered: an approximation technique based on the Pareto distribution and a spline approximation technique. Computational algorithms designed based on these techniques allow assessing ultra-low risks (on the order of 10–6–10–8) under the confirmed compliance of aircraft landing characteristics with airworthiness requirements. The modeling shows good agreement between the results obtained by these techniques, which makes it possible to implement a simpler technique based on the Pareto distribution. This technique reduces the amount of statistical modeling by predicting accuracy characteristics in the unobservable range of their variation.
作者简介
L. Aleksandrovskaya
Moscow State Aviation Technological University (MATI)
Email: Kirillinav@mati.ru
俄罗斯联邦, Moscow
A. Ardalionova
Moscow Institute of Electromechanics and Automatics (MIEA)
Email: Kirillinav@mati.ru
俄罗斯联邦, Moscow
A. Kirillin
Moscow State Aviation Technological University (MATI)
编辑信件的主要联系方式.
Email: Kirillinav@mati.ru
俄罗斯联邦, Moscow
![](/img/style/loading.gif)