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应用轨迹优化技术评估战斗机的功能敏捷性
引用本文:税清才,方振平.应用轨迹优化技术评估战斗机的功能敏捷性[J].航空学报,1996,17(4):456-459.
作者姓名:税清才  方振平
作者单位:北京航空航天大学509教研室,北京,100083
摘    要:应用三维轨迹优化方法 ,推导出最优操纵律完成 1 80°偏航机动。分析采用优化操纵策略对功能敏捷性的三种评估尺度 (战斗周期时间、动态速率转弯图和相对能量状态 )的影响。结果表明最优操纵策略可以最大限度地减少敏捷性评估尺度受飞行员操纵因素的影响 ,明显地改善战斗机的功能敏捷性

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收稿时间:1995-04-28;
修稿时间:1995-10-18

EVALUATION OF FUNCTIONAL AGILITY METRICS FOR AN ADVANCED FIGHTER AEROCRAFT USING TRAJECTORY OPTIMIZATION TECHNIQUES
Shui Qingcai,Fang Zhenping.EVALUATION OF FUNCTIONAL AGILITY METRICS FOR AN ADVANCED FIGHTER AEROCRAFT USING TRAJECTORY OPTIMIZATION TECHNIQUES[J].Acta Aeronautica et Astronautica Sinica,1996,17(4):456-459.
Authors:Shui Qingcai  Fang Zhenping
Institution:Faculty 509, Beijing University of Aeronautics and Astronautics, Beijing,100083
Abstract:An optimal control strategy deduced by means of three degree of freedom trajectory optimization techniques is used to achieve 180 degree heading changes of a fighter airplane. Three functional agility metrics such as combat cycle time,dynamic speed turn plots and relative energy state are analyzed. The effect of artificial control by pilot in evaluating functional agility metrics may be reduced to a great extent and significant improvements of agility metrics can be obtained by using an optimal maneuver.
Keywords:maneuverability  combat  dynamic control  trajectory optimization
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