| 战斗机功能敏捷性对操纵输入灵敏度的研究 |
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| 引用本文： | 税清才,方振平.战斗机功能敏捷性对操纵输入灵敏度的研究[J].北京航空航天大学学报,1995,21(3):22-28. |
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| 作者姓名： | 税清才 方振平 |
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| 作者单位： | 北京航空航天大学飞行器设计与应用力学系 |
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| 摘 要： | 提供了评估战斗机功能敏捷性的三种尺度──炸战周期时间，动态速率转弯图和相对能量状态，并以某机作为模型算例，用１８０°航向改机动动作，仿真计算了飞行员的操纵指令输入对功能敏捷性评估尺度的影响．算例模型包含了非线性全量运动方程，飞行控制系统和发动机的动力特性．因此，较为真实地反映了飞机的特性．
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| 关 键 词： | 歼击机 灵敏度 评价 操纵性 模拟仿真 |
ANALYSIS ON SENSITIVITY OF AGILITY METRICS TO THE PILOT CONTROL INPUTS FOR FIGHTER AIRCRAFT |
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| Shut Qingcai, Fang Zhenping.ANALYSIS ON SENSITIVITY OF AGILITY METRICS TO THE PILOT CONTROL INPUTS FOR FIGHTER AIRCRAFT[J].Journal of Beijing University of Aeronautics and Astronautics,1995,21(3):22-28. |
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| Authors: | Shut Qingcai Fang Zhenping |
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| Abstract: | Three metrics evaluating fighter functional agility are presented. The metrics are Combat Cycle Time. Dynamic Speed Turn plots and Relative Energy State. The sensitivity of these metrics to the pilot control command is explored using nonlinear. non-real-time-six-degree of freedom generic computer simulation for a fighter aircraft. The program is high fidelity, containing full control system, engine power and aerodynamic models. The maneuver test are 180 degree heading angle change. |
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| Keywords: | fighter aircraft sensitivity evaluations controllability (flight) analog simulation |
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