| 直升机机动性探讨 |
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| 引用本文： | 高正,孙传伟.直升机机动性探讨[J].南京航空航天大学学报,1997,29(6):666-673. |
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| 作者姓名： | 高正 孙传伟 |
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| 作者单位： | 南京航空航天大学直升机技术研究所 |
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| 摘 要： | 提出了直升机机动性的定性解释和定量评价参数，讨论了机动性对直升机效能的意义，论述了机动性与灵活性的关系以及影响机动性的设计参数，介绍了美国陆航设计标准中对直升机在频域响应方面的要求和试飞验证规定。文中举例分析了发动机／旋翼集成控制系统对提高机动性、改善飞行品质的应用，并指出自动控制理论和电子技术将对今后提高直升机的机动性起重要作用。
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| 关 键 词： | 直升机 操作性 设计参数 自动控制系统 机动性 |
Probing of Helicopter Maneuverability |
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| Gao Zheng,Sun Chuanwei.Probing of Helicopter Maneuverability[J].Journal of Nanjing University of Aeronautics & Astronautics,1997,29(6):666-673. |
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| Authors: | Gao Zheng Sun Chuanwei |
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| Abstract: | The qualitative explanation and the parameters for quantitative evaluation of helicopter maneuverability are presented. And also the affect of maneuverability on the mission efficiency of helicopters, the relationship between maneuverability and agility, and the design parameters which determine the maneuverability are discussed. This paper briefed the requirement for helicopter response in the frequency domain and the regulations of flight test in US Army ADS 33. Having the aid of some example of integral control system, this paper analyzed the importance of auto control theory and electronic technology for improving of helicopter maneuverability. |
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| Keywords: | helicopters maneuverability design parameters auto control system |
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