| 平飞时飞机机动载荷控制系统的分析和设计 |
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| 引用本文： | 徐军,陈微,王荣梅,张悦,刘杨.平飞时飞机机动载荷控制系统的分析和设计[J].飞行力学,2009,27(5). |
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| 作者姓名： | 徐军 陈微 王荣梅 张悦 刘杨 |
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| 作者单位： | 北京理工大学宇航科学技术学院; |
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| 摘 要： | 在基本飞机构型的条件下,给出机翼载荷控制的目的、方法和效能计算,研究了机动载荷控制系统的设计。通过对某型大展弦比飞机的设计和仿真,表明了控制系统对机翼载荷控制的有效性。
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| 关 键 词： | 载荷 机动 机动载荷控制 机翼弯度 |
Analysis and Design of Maneuvering Load Control System During Aircraft Level Flight |
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| XU Jun,CHEN Wei,WANG Rong-mei,ZHANG Yue,LIU Yang.Analysis and Design of Maneuvering Load Control System During Aircraft Level Flight[J].Flight Dynamics,2009,27(5). |
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| Authors: | XU Jun CHEN Wei WANG Rong-mei ZHANG Yue LIU Yang |
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| Institution: | School of Aerospace Science and Engineering;Beijing Institute of Technology;Beijing 100081;China |
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| Abstract: | Under basic aircraft configuration,the goal,control method and efficient computing of wing load control were presented.The design method of a maneuver load control system was researched.And it shows that the control system is efficient for wing load control through the design and simulation for the certain high-aspect-ratio composite aircraft. |
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| Keywords: | load maneuver maneuver load control wing bending |
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