首页 | 本学科首页   官方微博 | 高级检索  
     检索      

战斗机机敏性尺度评估的一种方法
引用本文:凌政国.战斗机机敏性尺度评估的一种方法[J].飞行力学,1992,10(2):1-7.
作者姓名:凌政国
作者单位:601所
摘    要:本文提出了一些机敏性度量尺度,研究了它们的分类,并试图对轴向和俯仰机敏性进行量化。用了功率攻击参数和功率损失参数量化轴向机敏性;用了上仰速率和下俯速率量化俯仰机敏性。因此,本文所引入的和所研究的内容可作为进一步研究机敏性时的参考和借鉴.

关 键 词:机敏性  过渡机敏性  歼击机

THE METHOD OF ASSESSMENT OF FIGHTER AGILITY METRICS
Ling Zhengguo.THE METHOD OF ASSESSMENT OF FIGHTER AGILITY METRICS[J].Flight Dynamics,1992,10(2):1-7.
Authors:Ling Zhengguo
Institution:60) Research Institute Ministry of Aeronautic and Astronautic Industry)
Abstract:This paper presents the retults of an analysis of proposed metrics to assess fight aircraft agility. A novel framework for classifying these metrics is developed and applied. A set of transient metrics intended to quantify the axial and pitch agility of fight aircraft is evaluated. Results indicate that the power onset and power loss parameters promising candidates for quantifying axial agility, while maximum pitch up and pitch down rates are for quantifying pitch agility.
Keywords:Agility Transient agility Functional agility Axial agility Power onset parameter Power less parameter
本文献已被 CNKI 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号