| 变后掠飞机受控动态响应的数值模拟 |
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| 引用本文： | 严明,邱传仁.变后掠飞机受控动态响应的数值模拟[J].上海交通大学学报,1986(6). |
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| 作者姓名： | 严明 邱传仁 |
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| 作者单位： | 上海交通大学工程力学系，上海交通大学工程力学系 |
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| 摘 要： | 变后掠飞机在变后掠过程中国气动外形的改变产生了飞机的固有变掠响应.在有驾驶员的操纵反应或自动驾驶仪的闭环控制时,飞机的受控变掠响应及相应控制规律的选择是值得研究的问题.本文给出了完整的变后掠飞机受控响应的数值模拟方法及算例.
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| 关 键 词： | 飞机 变后掠 飞行力学 控制 数值模拟 |
Simulation of Dynamic Response to Controlled Motion of an Aircraft with Variable-Geometry Wings |
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| Yan Ming, Qiu Chuanren.Simulation of Dynamic Response to Controlled Motion of an Aircraft with Variable-Geometry Wings[J].Journal of Shanghai Jiaotong University,1986(6). |
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| Authors: | Yan Ming Qiu Chuanren |
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| Institution: | Yan Ming; Qiu Chuanren |
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| Abstract: | In the course of changing the angle of sweep, the disturbances produced by the change of aerodynamic configuration induce a natural sweep changing response. In the case of manual control of pilot or closed loop control of autopilot, the response of the aircraft will be a controlled response, the characteristics of which as well as well as the selection of autocontrol law must be studied.
In this paper, a numerical method is presented for a complete solution of the controlled dynamic response of a variable sweep wing aircraft with autopilot, and some examples are given. |
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| Keywords: | airplane changing sweep flight mechanics control numerical simulation |
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