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航空发动机多模型预测滑模控制
苗卓广, 谢寿生, 王磊, 彭靖波, 翟旭升
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
DOI:
分类号:
基金项目:博士后科学基金(20100481498)。
Multi-Model Predictive Sliding Mode Control for Aero-Engine
MIAO Zhuo-guang, XIE Shou-sheng, WANG Lei, PENG Jing-bo, ZHAI Xu-sheng
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.
Key words:  Aero-engine  Multi-model  Sliding mode control  Predictive control  Flight envelope