| 飞行控制计算机电磁兼容正向设计方法 |
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| 引用本文： | 宁月光. 飞行控制计算机电磁兼容正向设计方法[J]. 仪表技术, 2014, 0(12): 28-30 |
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| 作者姓名： | 宁月光 |
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| 作者单位： | 海军装备部; |
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| 摘 要： | 提出一种飞行控制计算机的电磁兼容正向设计方法,在方案阶段根据系统需求进行预设计与风险评估,在功能研制阶段进行详细的滤波、接地设计,将电磁兼容设计融入到产品开发的各个方面,以期在降低成本的同时获得最佳的电磁兼容性能。
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| 关 键 词： | 电磁兼容 屏蔽 接地 滤波 |
A Forward Electromagnetic Compatibility Design Method of Flight Control Computer |
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| NING Yue-guang. A Forward Electromagnetic Compatibility Design Method of Flight Control Computer[J]. Instrumentation Technology, 2014, 0(12): 28-30 |
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| Authors: | NING Yue-guang |
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| Affiliation: | NING Yue-guang (Naval Equipment Department, Xi＇an 710043, China) |
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| Abstract: | In this paper, a forward design method for electromagnetic compatibility of flight control computer was described. According to the demand of system, pre-design and risk assessment should be accomplished in the scheme. A detailed design of filtering and grounding must be carried out during the research period of computer function. The elec- tromagnetic compatibility design was supposed to integrate into all aspects of the product development, in order to reduce the cost and achieve a better performance of electromagnetic compatibility |
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| Keywords: | electromagnetic compatibility shielding grounding filtering |
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