| 飞机盘旋/转弯机动研究 |
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| 引用本文： | 任志强,范国星.飞机盘旋/转弯机动研究[J].飞行力学,2010,28(2). |
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| 作者姓名： | 任志强 范国星 |
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| 作者单位： | 1. 中国人民解放军驻黎阳机械公司军代表室,贵州,安顺,561102
2. 中国人民解放军驻162厂军代表室,贵州,安顺,561000 |
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| 摘 要： | 利用飞机体轴系下的质点系动力学平衡方程和航迹轴系下的质点动力学平衡方程,将飞机的操纵性、定常性与机动性相结合,给出了飞机水平盘旋/转弯机动的分析方法。对某型飞机的分析结果表明,该方法在飞机设计中具有较高的使用价值。
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| 关 键 词： | 机动性 操纵性 稳定性 盘旋/转弯 |
Aircraft spiral/turning maneuver research |
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| REN Zhi-qiang,FAN Guo-xing.Aircraft spiral/turning maneuver research[J].Flight Dynamics,2010,28(2). |
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| Authors: | REN Zhi-qiang FAN Guo-xing |
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| Institution: | 1.In Liyang Machinery Company Military Representative Office of the PLA;Anshun 561102;China;2.In 162 Factories Military Representative Office of the PLA;Anshun 561000;China |
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| Abstract: | In this paper,the controllablity,stability and maneuverbility of aircraft are combined in the use of particle dynamics balance equation under an aircraft body and track shaft system.It provides the analysis method of research in aircraft level spiral/turning maneuver,and the analysis of a certain type of aircraft shows that the method has a higher value in aircraft design. |
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| Keywords: | maneuverbility controllablity stability spiral/turning |
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