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TVC/PSM飞机的过失速动态边界及敏捷性分析
引用本文:曹万里,沈宏良,刘昶.TVC/PSM飞机的过失速动态边界及敏捷性分析[J].飞行力学,2003,21(1):12-15.
作者姓名:曹万里  沈宏良  刘昶
作者单位:南京航空航天大学空气动力学系,江苏南京,210016
摘    要:以飞机为质点,考虑在最少输入数据情况下,曲于转弯速率图并从能量的角度计算和分析了TVC/PSM飞机的过失速动态边界,选取敏捷性尺度空战周期时间和指向裕度,对比分析了TVC/PSM飞机和传统飞机的敏捷性,得出了一些有益的结论,并提出了一些建议。

关 键 词:TVC  PSM  敏捷性  推力矢量控制  过失速机动  战斗机
文章编号:1002-0853(2003)01-0012-04
修稿时间:2002年4月1日

Post Stall Dynamic Boundaries and Agility Analysis of TVC/PSM Aircraft
CAO Wan li,SHEN Hong liang,LIU Chang.Post Stall Dynamic Boundaries and Agility Analysis of TVC/PSM Aircraft[J].Flight Dynamics,2003,21(1):12-15.
Authors:CAO Wan li  SHEN Hong liang  LIU Chang
Abstract:Considering the aircraft as particle and using minimal input data to analyze the agility and post stall dynamic boundaries of TVC/PSM aircraft, which based on the analysis of turn rate plot and energy information. Some agility metrics, such as combat cycle time(CCT) and point margin(PM), were selected to compare and analyze the agility between TVC/PSM aircraft and conventional aircraft and some valuable conclusion and suggestion were arrived at in the end.
Keywords:agility  thrust vector control  post stall maneuver
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