| 飞机操纵系统舵机与助力器运动碰撞研究 |
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| 引用本文： | 王艺兵,王占林.飞机操纵系统舵机与助力器运动碰撞研究[J].航空学报,1998,19(3):365-370. |
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| 作者姓名： | 王艺兵 王占林 |
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| 作者单位： | 1. 青岛大学, 青岛, 266071;2. 北京航空航天大学303 教研室, 北京, 100083 |
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| 摘 要： | 飞机操纵系统中因舵机输出较快，助力器响应较慢而存在相互运动碰撞，影响操纵品质和飞行安全。对发生碰撞的机理进行了深入分析，建立了舵机与助力器运动特性匹配关系和用于碰撞研究的数学模型，通过实例，找到了对碰撞最有影响的参量。
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| 关 键 词： | 飞机操纵系统 舵机 助力器 碰撞 |
| 收稿时间： | 1997-08-16 |
| 修稿时间： | 1998-01-20 |
STUDY OF COLLISION BETWEEN SERVO MECHANISM AND BOOSTER IN CONTROL SYSTEMS OF AIRCRAFT |
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| Wang Yibing,Wang Zhanlin.STUDY OF COLLISION BETWEEN SERVO MECHANISM AND BOOSTER IN CONTROL SYSTEMS OF AIRCRAFT[J].Acta Aeronautica et Astronautica Sinica,1998,19(3):365-370. |
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| Authors: | Wang Yibing Wang Zhanlin |
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| Institution: | 1. Qingdao University,Qingdao,266071;2. Faculty 303, Beijing University of Aeronautics and Astronautics,Beijing,100083 |
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| Abstract: | Because of the slower response of a booster than that of a servomechanism, collision exists in the aircraft′s control system. It affects the performance and flight safety. The reason and originality are analysed. A mathematical model is built. By the example, the most effective parameters are found and the way to eliminate collision is also obtained. WT5”HZ〗 |
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| Keywords: | mechanical control system servomechanism booster collision |
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