| 引用本文: | 廖瑛,王京.某巡航式飞行器控制系统设计与仿真.[J].国防科技大学学报,2001,23(6):24-27.[点击复制] |
| LIAO Ying,WANG Jing.The Design and Simulation of A Cruise Aircraft Control System[J].Journal of National University of Defense Technology,2001,23(6):24-27[点击复制] |
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| 某巡航式飞行器控制系统设计与仿真 |
| 廖瑛, 王京 |
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(国防科技大学 航天与材料工程学院, 湖南 长沙 410073)
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| 摘要: |
| 在详细分析某巡航式飞行器运动模型的基础上，论述了采用经典控制理论设计该飞行器控制系统的方法，并在考虑限幅、延迟等非线性环节的基础上，进一步对控制系统参数进行了仿真分析。通过部分仿真结果曲线可以看出，控制系统结构和参数合理，可以满足该飞行器控制的总体性能要求。同时，可以为控制系统的半实物仿真及实际飞行提供更为可信的参考数据及曲线。 |
| 关键词: 巡航飞行 控制系统设计 计算机仿真 |
| DOI： |
| 投稿日期：2001-09-15 |
| 基金项目:国家863基金资助项目（863-2-5-2.4） |
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| The Design and Simulation of A Cruise Aircraft Control System |
| LIAO Ying, WANG Jing |
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(College of Aerospace and Materials Engineering,National Univ. of Defense Technology, Changsha 410073,China)
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| Abstract: |
| This paper mainly describes the method of designing a aircraft control system based on the classical control theory after creating the aircraft movement models. The control system's performance is also simulated with the effects of some nonlinear elements such as saturation and transport delay. From the results we can see that the structure and parameters are reasonable, the performance can meet the need of the task. At the same time, it can offer more creditable data and diagram for the hardware-in-the-loop simulation and the flight experiment. |
| Keywords: cruise flight design of control system computer simulation |
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