| 基于飞控系统故障后的飞行品质评定方法适航验证技术研究 |
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| 引用本文： | 王育平、徐南波.基于飞控系统故障后的飞行品质评定方法适航验证技术研究[J].民用飞机设计与研究,2013(3):19. |
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| 作者姓名： | 王育平、徐南波 |
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| 作者单位： | 上海飞机设计研究院,上海,201210 |
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| 摘 要： | 使用电子飞行控制系统的运输类飞机必须要满足适航安全性的要求。由于运输类飞机通用的规章(14CFAR25部)中许多稳定性和操纵性的要求已经不能代表和覆盖对这类飞机的最低安全要求，因此需要采用新的适航验证方法进行适航评定。通过对某型飞机的研究，采用HQRM方法评定，给出了分析取证的流程以及思路，最后给出按照不同组合概率选取不同的适航验证方案。
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| 关 键 词： | 操纵品质评定等级 电子飞行控制系统 运输类飞机 |
Research on Airworthiness Certification Technology Based on Handling Qualities Rating Method after Flight Control System Failure |
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| Wang Yuping
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Xu Nanbo.Research on Airworthiness Certification Technology Based on Handling Qualities Rating Method after Flight Control System Failure[J].Civil Aircraft Design and Research,2013(3):19. |
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| Authors: | Wang Yuping Xu Nanbo |
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| Institution: | Shanghai Aircraft Design and Research Institute,Shanghai 201210,China |
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| Abstract: | The transport category airplanes employing electronic flight control systems (EFCS) must meet the requirements of safety. As the stability and control requirements in the regulations for transport aircraft (14 CFAR25) hasn't been able to stand for and cover with the lest safe requirements for such aircraft, a new method of airworthiness certification need to be used for airworthiness assessment. This paper provides some produces and ideas for compliance through studying a certain airplane with Handling Qualities Rating Method (HQRM). |
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| Keywords: | Handling Qualities Rating Method ( HQRM ) Electronic Flight Control Systems Transport Category Airplanes |
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