| IFSTA自主着舰控制律仿真研究 |
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| 引用本文： | 华艺欣,王海平,曹良秋.IFSTA自主着舰控制律仿真研究[J].飞行力学,2016(6):30-33. |
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| 作者姓名： | 华艺欣 王海平 曹良秋 |
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| 作者单位： | 1. 中国飞行试验研究院飞机所,陕西西安,710089;2. 中国飞行试验研究院科技部,陕西西安,710089 |
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| 摘 要： | 针对舰载机的自动着舰系统,以IESTA原型机K8飞机为研究对象建立了着舰环境模型,设计了自动着舰控制律,对在着舰阶段的控制作用及影响着舰精度的因素进行了分析和研究,并分别进行了数值仿真和半实物地面仿真验证.研究结果表明,为了使飞机成功完成着舰任务,需满足海况、大气扰动、控制系统带宽频率的最低要求.
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| 关 键 词： | IFSTA 自动着舰系统 推力补偿控制 半实物地面仿真 |
Research of automatic carrier landing control law simulation by IFSTA |
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| Abstract: | In this paper,automatic carrier landing system of carrier-based aircraft is introduced.Model of landing circumstance is established which is based on the prototype model of IFSTA-K8,and auto landing control law is designed.Control effect during landing process and factors which influence landing precision are studied.At last,numerical simulation and semi-physical ground simulation are both performed.These results demonstrate that in order to land on board successfully,the minimum requirements of sea condition,atmospheric disturbance and control system band frequency should be met. |
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| Keywords: | IFSTA automatic carrier landing system power compensation control semi-physical ground simulation |
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