| 直升机着舰飞行控制仿真研究初探 |
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| 引用本文： | 吴文晓,徐明.直升机着舰飞行控制仿真研究初探[J].直升机技术,1999(1). |
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| 作者姓名： | 吴文晓 徐明 |
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| 作者单位： | 海军特种飞机论证研究所，海军特种飞机论证研究所 上海 200436，上海 200436 |
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| 摘 要： | 本文介绍了直升机的着舰过程和特点,以及舰船运动特性及其对直升机着舰的影响,分析了着舰飞行控制系统在着舰过程各个阶段的不同任务和要求,最后提出一种着舰飞行控制系统的设计方法和一个很好的仿真工具。
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| 关 键 词： | 飞行控制 着舰 LQG/LTR方法 |
PRIMARY INVESTIGATION ON FLIGHT CONTROL SIMULATION OF A HELICOPTER LANDING ON SHIP |
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| Authors: | Wu Wenxiao Xu Ming |
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| Abstract: | This paper introduces the process and characteristics of a helicopter landing,and analyses the characteristics of ship motions and the influnence of ship motions to helicopter landing.Then,the different tasks and requests of embarked helicopter flight control system in the process of landing are describeed.At last,the paper brings forword a method to design the flight control system of landing and an advanced simulation tool. |
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| Keywords: | flight control embarked LQG/LTR method |
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