航空电子设备标度规律的实证研究

B. Annighoefer, Vitaly Posternak, F. Thielecke
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引用次数: 1

摘要

本文进行了一项实证研究,得出了飞行器性能与航空电子系统之间的定量关系。利用现有的优化方法,对大量飞行器和通用航电平台的航电系统进行了优化计算。提出了一套基本且易于确定的飞行器性能,用以表征飞行器并驱动航空电子系统。例如I/ o的实例数及其空间范围。根据车辆的基本性能对其进行分类、优化并对结果进行分析,从而使每个车辆特性的影响以及不同航电平台的重量变得可量化。通过插值法,导出了将飞行器特性任意值与航电平台重量联系起来的简单数学方程,即标度定律。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Empirical investigations on avionics scaling laws
This article presents an empirical study deriving quantitative relations between vehicle properties and avionics systems. Existing optimization methods are used to calculate the optimal avionics systems for a great number of vehicles as well as common avionics platforms. A set of basic and easy-to-determine vehicle properties is suggested, which characterize the vehicle and drive the avionics system. For instance number of I/Os and their spatial extent. Vehicles are classified by their basic properties, optimized and the results are analyzed such that the effect of each individual characteristic vehicle property and the resulting weight for different avionics platforms becomes quantifiable. By interpolation simple mathematical equations are derived, which relate arbitrary values of characteristic vehicle properties with the weight of avionics platforms, so called scaling laws.
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