...
首页> 外文期刊>International journal of systems assurance engineering and management >Application of probability distributions mixture of safety indicator in risk assessment problems
【24h】

Application of probability distributions mixture of safety indicator in risk assessment problems

机译:安全指标的概率分布混合在风险评估中的应用

获取原文
获取原文并翻译 | 示例

摘要

The main indicator of quality functioning of the aircraft pilotage system is flight safety. Thereby, in accordance with acceptable risk concept, demands with safety indicators are being determined in probability form and circumferential acceptable risk values could be very small order of magnitude 1~(-6)-10~(-8). Such demands for the precision characteristics of vertical echeloning and automatic landing of civil aircrafts are valid during flights in all weather conditions. At certification of aircrafts these demands should be confirmed. Thereto, the only possible way of demand confirmation with such small risks is statistical mathematical modeling in the wast range of disturbing factors. Mathematical modeling is inseparable part of aircraft piloting system development and it is accepted as legitimate at corresponding verification, which enables the guarantee for adequate aircraft movement modeling. The most complete information about aircraft movement probability characteristics is contained within laws of their probability distributions. In classical mathematical statistics papers there is no investigations of very small and very big probabilities. Therefore for solving the safety problems, connected with needs for investigation "tail" (last) distribution parts, necessary to develop a new methods. One of them is presented into this paper. For problems of statistical modeling of aircraft movement in the wast range of disturbing factors the typical appearance of "breach"— distribution law alteration of analyzed parameters. The cause of the "breach" is realization of unlikely extreme values of disturbed random factors and their mixtures at large quantities of modeling, which reconduct corresponding systems in areas of nonlinearity. It is mentioned that the effect of "breach" is characteristical not only for problems of aircraft piloting but also for the wast range of problems in different practice applied areas—ecology, quality management (Six Sigma methodology) and other.
机译:飞机引航系统质量运行的主要指标是飞行安全。因此,根据可接受的风险概念,以概率形式确定具有安全指标的需求,并且周向可接受的风险值可能非常小,数量级为1〜(-6)-10〜(-8)。在所有天气条件下的飞行过程中,对垂直飞行和民用飞机自动着陆的精度特性的这种要求是有效的。在飞机合格审定中,这些要求应予以确认。迄今为止,具有如此小的风险的需求确认的唯一可能方法是在干扰因素的浪费范围内进行统计数学建模。数学建模是飞机驾驶系统开发不可分割的一部分,在相应的验证中它被认为是合法的,这可以保证飞机有足够的运动建模。有关飞机运动概率特征的最完整信息包含在其概率分布定律之内。在经典的数学统计论文中,没有关于很小和很大概率的研究。因此,为解决安全问题,与调查“尾部”(最后)配电部件的需求相关,有必要开发一种新方法。本文介绍了其中之一。对于干扰因素浪费范围内的飞机运动统计建模问题,通常会出现“违反”的现象,即分析参数的分布规律改变。 “突破”的原因是,在大量建模中,受干扰的随机因素及其混合的极不可能出现极值,从而在非线性区域中重构了相应的系统。提到“突破”的影响不仅对于飞机驾驶问题是特征性的,而且对于生态,质量管理(六西格码方法论)等其他不同实践应用领域中的问题浪费也很典型。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号