涡轴发动机导叶控制系统建模仿真及其PID控制器改进

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

基金项目: 航空支撑科技基金(04B52006)

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出版历程
- 收稿日期: 2011-08-10
- 修回日期: 2011-10-08
- 刊出日期: 2011-11-28

Modeling simulation of turboshaft engine IGV digital control system and PID controller improvement

摘要

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:响应迅速,无振荡,仅有很小超调,满足了系统研制性能要求.
- 涡轴发动机 /
- 导叶控制系统 /
- 数学模型 /
- 建模仿真 /
- PID控制器
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.
- turboshaft engine /
- IGV(inlet guide vane) control system /

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参考文献(12)

[1]	姚文荣,孙健国.基于在线可变导叶角的涡轴发动机优化控制[J].航空动力学报,2007,22(11):1930-1934. YAO Wenrong,SUN Jianguo.Online optimization control of turboshaft engines based on variable inlet guide vane[J]. Journal of Aerospace Power, 2007,22(11):1930-1934. (in Chinese)
[2]	Smith R H, Chisholm J D, Stewart J F. Optimizing aircraft performance with adaptive, integrated flight/propulsion control[J]. Journal of Engineering for Gas Turbine and Power,1991,113(1):87-92.
[3]	Gastineau Z.Robust internal model turbomachinery control .Dallas,Texas:Mechanical Engineering Department, Southern Methodist University,1998.
[4]	Sun J, Elder R L.Numerical optimization of a stator vane setting in multistage axial-flow compressor[J].Journal of Power and Energy,1998,212(4):247-259.
[5]	熊劲松,侯安平,袁巍,等.可调叶片的发展趋势及其气动问题的探讨[J].航空动力学报,2008,23(1):112-116. XIONG Jinsong, HOU Anping, YUAN Wei, et al.Some discuss on technology trend and aerodynamics problem of adjustable blade[J].Journal of Aerospace Power,2008,23(1):112-116.(in Chinese).
[6]	邓文革、文建彬.航空发动机导叶数控装置 .北京:中航总公司发动机自控学会学术讨论会,1992.
[7]	邓文革.某型发动机双通道数字式导叶控制器研究 .西安:中航总公司发动机自控学会学术讨论会,1998.
[8]	王占林.液压伺服控制[M].北京:北京航空学院出版社, 1987.
[9]	李玥,健国.基于遗传算法的航空发动机多目标优化PID控制[J].航空动力学报,2008,23(1):174-178. LI Yue,SUN Jianguo.Multi-objective optimization of aeroengine PID control based on multi-objective genetic algorithms[J].Journal of Aerospace Power,2008,23(1):174-178.(in Chinese)
[10]	吴勇,谢寿生,唐奇,等. 基于支持向量机的航空发动机PID 解耦控制[J].航空动力学报,2009,24(10):2349-2355. WU Yong,XIE Shousheng,TANG Qi,et al.PID decoupling controller for aero-engine based on support vector machines[J].Journal of Aerospace Power,2009,24(10):2349-2355.(in Chinese)
[11]	陈金醮.计算机控制技术[M].长沙:中南工业大学出版社, 1990.
[12]	陈建铎.Intel单片机应用技术[M].西安:陕西科学技术出版社,1991.