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| 涡轴发动机导叶控制系统建模仿真及其PID控制器改进 | |
| 引用本文： | 周剑波,邓文革,刘铁庚,孙健国.涡轴发动机导叶控制系统建模仿真及其PID控制器改进[J].航空动力学报,2011,26(11):2578-2583. |
| 作者姓名： | 周剑波 邓文革 刘铁庚 孙健国 |
| 作者单位： | 1. 南京航空航天大学能源与动力学院,南京210016／中国航空工业集团公司中国航空动力机械研究所,湖南株洲412002 2. 中国航空工业集团公司中国航空动力机械研究所,湖南株洲,412002 3. 南京航空航天大学能源与动力学院,南京,210016 |
| 基金项目： | 航空支撑科技基金(04B52006) |
| 摘 要： | 通过对航空涡轴发动机数字式导叶控制系统各个环节分析计算,建立了系统的数学模型,在系统仿真分析的基础上,对PID（proportion integral derivative）控制器进行了改进设计,提出了不完全微分先行二阶PID控制方法.试验结果表明,使用不完全微分先行二阶PID控制方法,导叶控制系统性能明显改善：响应迅... |
| 关 键 词： | 涡轴发动机 导叶控制系统 数学模型 建模仿真 PID控制器 |
| 收稿时间： | 2011/8/10 0:00:00 |
| 修稿时间： | 2011/10/8 0:00:00 |
Modeling simulation of turboshaft engine IGV digital control system and PID controller improvement |
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| ZHOU Jian-bo,DENG Wen-ge,LIU Tie-geng and SUN Jian-guo.Modeling simulation of turboshaft engine IGV digital control system and PID controller improvement[J].Journal of Aerospace Power,2011,26(11):2578-2583. | |
| Authors: | ZHOU Jian-bo DENG Wen-ge LIU Tie-geng and SUN Jian-guo |
| Institution: | ZHOU Jian-bo1,2,DENG Wen-ge2,LIU Tie-geng2,SUN Jian-guo1 (1.College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China,2.China Aviation Powerplant Research Institute,Aviation Industry Corporation of China,Zhuzhou Hunan 412002,China) |
| Abstract: | Simulation of turboshaft engine IGV (inlet guide vane) digital control system was performed with system model,which was obtained through analysis and calculation.PID(proportion integral derivative) controller of IGV was improved based on the above work and a method called predetermined incomplete differential of the second order PID control was proposed.Test results show that the IGV digital control system is improved obviously.The response is more quick without oscillation,and agrees with the design requirements. |
| Keywords: | turboshaft engine IGV(inlet guide vane) control system |
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