| 功能敏捷性评估与影响因素研究 |
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| 引用本文： | 尹江辉 刘昶. 功能敏捷性评估与影响因素研究[J]. 飞行力学, 1995, 13(2): 33-39 |
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| 作者姓名： | 尹江辉 刘昶 |
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| 作者单位： | 南京航空航天大学 |
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| 摘 要： | 建立了现代高机动性能战斗机功能敏捷性仿真计算数学模型，并以Ｆ－１６战斗机为例，对其功能敏捷性尺度－－空战周期时间和相对能量状态进行了数字仿真研究。结果表明，不同初始飞行状态对飞机功能敏捷性有显著影响，改善和提高发动机性能，合理设计和选取飞机的控制系统和机动飞行中的操纵动作，将有利于发挥飞机敏捷性功能。
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| 关 键 词： | 功能敏捷性 空战周期时间 歼击机 操纵性 |
A STUDY OF ASSESSMENT AND EFFECTIVENESS OF FIGHTER FUNCTION AGILITY |
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| Yin Jianghui , Liu Chang,Zhen Xianfeng. A STUDY OF ASSESSMENT AND EFFECTIVENESS OF FIGHTER FUNCTION AGILITY[J]. Flight Dynamics, 1995, 13(2): 33-39 |
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| Authors: | Yin Jianghui Liu Chang Zhen Xianfeng |
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| Affiliation: | Nanjing University of Aeronautics and Astronautics |
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| Abstract: | Mathematical model for simulation calculating the function agility of modernhigh maneuveable fighter is established in this paper. The function agility metrics of a sampleF 16 fighter, such as combat cycle time and relative energy state are numbericallysimulated. The results show that the initial conditions have natable effect on fighter functionagility , and improving the performance of engine , reasonably designing and choosing thecontrol system and the control laws in maneuvering flight will be benefit to develop functionagility of fighter. |
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| Keywords: | Function agility Combat cycle time Relative energ state |
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