现代战斗机系统集成过程中的电磁干扰问题——一个案例研究

N.S. Chandrasekhar, T. Parthasarathy, P. Rao
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引用次数: 0

摘要

只提供摘要形式。现代战斗机是一个电子密集型武器平台,伴随有电磁干扰问题。数字飞线飞行控制系统、电子前轮转向和制动管理系统以及数字发动机控制系统的使用加剧了这个问题。所有这些系统都是安全关键,由于机载电子系统或外部电磁环境的电磁干扰,这些系统发生故障将导致飞机损失。印度轻型战斗机(LCA)采用了所有现代技术,必须设计确保电磁干扰问题最小化。电磁兼容工程是整个飞机设计、制造和测试的一部分。这包括制定和实施一个综合的电磁干扰控制计划,包括子系统和系统级的各种电磁兼容指导方针。特殊的EMC功能包括使用单接地参考点(SGRP)概念的混合接地系统,其中返回电流(功率和信号)不流经飞机结构,从而消除了低频时麻烦的共模接地环路耦合。EMC分析和预测技术在项目早期定义阶段用于所有天线的最佳位置,以最大限度地减少机载各种射频系统之间的相互干扰。严格执行符合MIL-STD-461C的LRU级试验计划,在机级分析豁免对其他系统的影响后,才准予豁免。飞机级系统内和系统间电磁兼容测试正在进行中。由于系统的电磁干扰分析、设计和测试方法在各个层面上,在飞机系统集成和测试阶段观察到很少的电磁干扰问题,目前已进入后期阶段。然而,在系统集成过程中发现的一些问题,采用电磁干扰修复方法得到了解决。本文介绍了LCS采用的电磁兼容设计与分析技术、系统集成阶段进行的电磁干扰测试、系统集成过程中遇到的电磁干扰问题、问题分析及解决方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
EMI problems during system integration of a modern fighter aircraft-a case study
Summary form only given. A modern fighter aircraft is an electronics-intensive weapon platform with attendant EMI problems. The problem is exacerbated by the use of digital fly by wire flight control system, electronics nose wheel steering and brake management systems, and digital engine control systems. All these systems are safety critical and malfunctioning of these systems due to EMI from onboard electronics systems or due to external electromagnetic environment would lead to loss of aircraft. The Indian Light Combat Aircraft (LCA) which incorporates all the modern technologies has to be designed to ensure that the EMI problems are minimised. EMC engineering was adopted as part of the overall aircraft design, fabrication and testing. This includes formulation and implementation of a comprehensive EMI control plan incorporating various EMC guidelines at subsystem level and system level. Special EMC features include a hybrid grounding system using Single Ground Reference Point (SGRP) concept wherein the return current (power and signal) do not flow through the aircraft structure resulting in elimination of the troublesome common mode ground loop coupling at low frequencies. EMC analysis and prediction techniques were used at the early project definition phase for optimum location of all antennas to minimise mutual interference between various RF system onboard aircraft. Test Plan at LRU level conforming to MIL-STD-461C was strictly enforced and waivers were granted only after aircraft level analysis of the effect of waiver on other system. Aircraft level intra system and inter system EMC Tests are now in progress. As a result of systematic EMC analysis, design and test methodologies at various levels, very few EMI problems were observed during aircraft system integration and testing phase which is now in an advanced stage. However, a few problems which were discovered during the system integration were solved using the EMI Fix method. This paper describes the EMC design and analysis techniques adopted, the EMI tests conducted during the system integration phase of LCS, the EMI problems faced during the system integration, analysis of the problems and the solution to the EMI problems.
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