| 飞行与推力综合控制系统的设计 |
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| 引用本文： | 王凯,章卫国.飞行与推力综合控制系统的设计[J].飞行力学,1997,15(1):56-59. |
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| 作者姓名： | 王凯 章卫国 |
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| 作者单位： | 西北工业大学!西安，710072 |
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| 摘 要： | 讨论了一种具有飞行与推力综合舰载机自动着舰控制系统的设计方法。结合国产某型收音机首先分析了基于俯仰姿态的升降速率控制系统的结构与控制规律；然后，对飞机进场功率补诉结构与控制规律进行了分析；最后，在同时考虑飞行控制系统与发动机推力补偿控制系统的条件下，对该综合系统的控制规律进行了设计与仿真，并提供了仿真结果。
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| 关 键 词： | 飞行控制 推力控制 综合系统 舰载机 |
Design of the Integrated Flight and Thrust Control Systems |
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| Wang Kai,Zhang Weiguo,Shi Zhongke.Design of the Integrated Flight and Thrust Control Systems[J].Flight Dynamics,1997,15(1):56-59. |
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| Authors: | Wang Kai Zhang Weiguo Shi Zhongke |
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| Institution: | Northwestern Polytechnical University |
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| Abstract: | A design method of the automatic control systems with Integrated flight and thrust controls for landing on carrier is discussed in this paper. The paper first analyzes the longitudinal flight control system and designs the h-Dot control law based on the pitch attitude; then, analyzes the control law of the power compensation system for landing approach;and finally, designs the control laws of the Integrated system. The simulation results are also provided. |
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| Keywords: | Flight control Thrust control Integrated system Aircraft on carrier Automatic landing on carrier |
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