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航空发动机分布式系统解耦控制研究
引用本文:段进峰,彭靖波,谢寿生,王立国.航空发动机分布式系统解耦控制研究[J].火力与指挥控制,2017,42(5).
作者姓名:段进峰  彭靖波  谢寿生  王立国
作者单位:1. 空军工程大学航空航天工程学院,西安,710038;2. 解放军95507部队,贵阳,550000
基金项目:国家自然科学基金,陕西省自然科学基础研究计划青年人才基金资助项目
摘    要:航空发动机控制系统是一个复杂的多变量控制系统,控制变量之间的相互耦合会严重影响系统的动态、稳态性能,在发动机最大工作状态时,甚至会造成超温、超转等现象,严重威胁着飞行安全,制约着发动机性能的提高。针对上述情况,利用改进型遗传算法对航空发动机双回路PID控制参数进行寻优,实现了对控制变量的解耦。数值仿真结果表明改进方法能有效消除各变量之间的耦合影响,而且在控制精度、跟踪性能等方面表现良好,对不同环境条件下的航空发动机模型均有良好的控制效果,适用于航空发动机控制。

关 键 词:航空发动机  分布式控制  模拟退火  自适应遗传算法  解耦

Research on Decoupling Method for Distribute Control of Aero-engine
DUAN Jin-feng,PENG Jing-bo,XIE Shou-sheng,WANG Li-guo.Research on Decoupling Method for Distribute Control of Aero-engine[J].Fire Control & Command Control,2017,42(5).
Authors:DUAN Jin-feng  PENG Jing-bo  XIE Shou-sheng  WANG Li-guo
Abstract:Aero-engine control system is quite a complicated multivariable system with its variables coupling each other which will impact on the static and dynamic performance of system and even will give rise to the phenomena of exceeding temperature or rev in its ultimate state which not only threats the flight safety severely but also restrict the advance of Aero-engine's performance.To solve this problem,a PID decoupling controller based on improved genetic algorithm is presented.The digital simulation of the control system has proved its excellent performance in controlling precision and tracking.The method is suitable for the aero-engine control system since it can assure satisfactory transient performance of aero-engine in condition of different environment and alleviate the coupling influence of each control variable effectively.
Keywords:Aero-engine  Distributed control  Simulated annealing  Adaptive genetic algorithm  Decoupling
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