| 机动增强及阵风减缓飞行控制系统设计 |
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| 引用本文： | 杨一栋,王建平.机动增强及阵风减缓飞行控制系统设计[J].航空学报,1987,8(4):171-178. |
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| 作者姓名： | 杨一栋 王建平 |
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| 作者单位： | 南京航空学院 |
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| 摘 要： | 本文以CCV—YF—16飞机为背景,阐述了机动增强/阵风减缓这一直接力控制模态的构成及设计思想;以数字仿真进行功能验证与评价;提出以C飞行品质指标为目标函数的参数优化设计法,从而有效地解决该模态的参数设计问题。
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| 收稿时间： | 1986-06-25; |
DESIGN OF FLIGHT CONTROL SYSTEM WITH MANEUVER ENHANCEMENT AND GUST ALLEVIATION |
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| Yang Yidong,Wang Jianping.DESIGN OF FLIGHT CONTROL SYSTEM WITH MANEUVER ENHANCEMENT AND GUST ALLEVIATION[J].Acta Aeronautica et Astronautica Sinica,1987,8(4):171-178. |
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| Authors: | Yang Yidong Wang Jianping |
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| Institution: | Nanjing Aeronautical Insitute |
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| Abstract: | This paper, based on the CCU-YH-16 fighter aircraft,investigates the design philosophy and configuration of the.flight control system with maneuver enhancement and gust alleviation. Comparison between basic flight control system and maneuver enhancement/gust alleviation system is shown by simu lation results.The functions of maneuver enhancement/gust alleviation are examined and evaluated.Parameter optimization method is used using C* flight performance criterion as objective function. |
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