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航空发动机多模型预测滑模控制
引用本文:苗卓广,谢寿生,王磊,彭靖波,翟旭升. 航空发动机多模型预测滑模控制[J]. 推进技术, 2012, 33(3): 472-477
作者姓名:苗卓广  谢寿生  王磊  彭靖波  翟旭升
作者单位:空军工程大学工程学院,陕西西安,710038
摘    要:针对航空发动机是一个不确定性的强非线性系统,借鉴多模型方法和预测控制思想,提出了航空发动机多模型预测滑模控制。对航空发动机飞行包线进行划分,建立了航空发动机状态空间多模型;对每个模型分别设计了预测滑模控制器,以滑模轨迹为预测模型,进行滚动优化、反馈校正求取控制量,并根据前几时刻与发动机的匹配程度选择当前时刻的控制器;推导出了其稳定性的条件。仿真结果表明,所设计的控制器控制效果令人满意,能有效抑制参数摄动和干扰的影响。

关 键 词:航空发动机  多模型  滑模控制  预测控制  飞行包线
收稿时间:2011-06-16
修稿时间:2011-11-19

Multi-Model Predictive Sliding Mode Control for Aero-Engine
MIAO Zhuo-guang,XIE Shou-sheng,WANG Lei,PENG Jing-bo and ZHAI Xu-sheng. Multi-Model Predictive Sliding Mode Control for Aero-Engine[J]. Journal of Propulsion Technology, 2012, 33(3): 472-477
Authors:MIAO Zhuo-guang  XIE Shou-sheng  WANG Lei  PENG Jing-bo  ZHAI Xu-sheng
Affiliation:(Engineering Institute,Air Force Engineering University,Xi’an 710038,China)
Abstract:A method of multi-model predictive sliding mode control was put forward for aero-engine with uncertainty and strong nonlinearity.The method drew lessons from the ideology of multi-model and predictive control.Firstly,the flight envelope of a certain aero-engine was plotted,and the state space multi-models were established.Secondly,predictive sliding mode controller was separately designed for each model.The algorithm predicted future sliding mode values and made rolling optimization and feed-back correction to get the control value.The current controller was chosen based on the match degree of outputs between the models and the aero-engine.Lastly,the stability condition was deduced.Simulation results show that the devised controller has good effect and restrains the influence of parameters perturbation and interfere.
Keywords:Aero-engine  Multi-model  Sliding mode control  Predictive control  Flight envelope
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