| 飞机横侧响应反馈控制律设计 |
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| 引用本文： | 盛小明.飞机横侧响应反馈控制律设计[J].飞行力学,1995,13(3):61-67. |
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| 作者姓名： | 盛小明 |
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| 摘 要： | 以某原型机为例对三自由度电传系统横侧响应反馈控制律的设计原理及计算方法进行了探讨，所提出的参数顶修正法能使指标检验与系统控制参数调整构成稳定闭环，进一步提高了匹配精度。经数字仿真和实时仿真试验证明，所提出的方法能够满足总体要求。
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| 关 键 词： | 飞行控制 控制律设计 响应反馈 |
RESEARCH FOR THE AIRAFT LATERAL-DIRECTIONAL RESPONSE FEEDBACK CONTROL LAW DESIGN |
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| Sheng Xiaoming.RESEARCH FOR THE AIRAFT LATERAL-DIRECTIONAL RESPONSE FEEDBACK CONTROL LAW DESIGN[J].Flight Dynamics,1995,13(3):61-67. |
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| Authors: | Sheng Xiaoming |
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| Institution: | 609 Research Institute Ministry of Aeronautic and Astronautic Industry |
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| Abstract: | The lateral-directional control law of response feedback for the three-free degree digital fly-by-wire system of a certain of basic aircraft has been investigated in this paper.A matching method,called parameter pre-modified technique(PPM), which can compose a stable closed-loop between error checking and parameters adjusting of the system and can improve the matching precision greatly,has been proposed.The property and the effectiveness of the PPM technique has been proved out by the digital and real-timesimulation. |
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| Keywords: | Flight control Fly-by-wire The design of control lawResponse feedback |
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