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Research on nonlinear model predictive control for turboshaft engines based on double engines torques matching

Research on nonlinear model predictive control for turboshaft engines based on double engines torques matching
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摘要 In order to reach a compromise between fast response control and torques matching control in double turboshaft engines,research on nonlinear model predictive control for turboshaft engines based on double engines torques matching is conducted.Meanwhile,a Nonlinear Model Predictive Control(NMPC)method is proposed,which combines the control index of the power turbine speed with torques matching of double engines creatively.In addition to the control index,the difference of output torques between each engine is also incorporated in the objective function as a penalty term to ensure constant speed control and short torques matching time.Simulation results demonstrate that relative to unilateral torques matching,the settling time of the bidirectional matching method can be reduced by nearly 30.8%.Nevertheless,compared with the bidirectional torques matching method under the cascade PID controller,the NMPC method can decrease the overshoot of the power turbine speed by 65%and reduce the matching time by 15.5%synchronously.Besides fast response control of turboshaft engines,fast torques matching control of double engines is accomplished as well. In order to reach a compromise between fast response control and torques matching control in double turboshaft engines,research on nonlinear model predictive control for turboshaft engines based on double engines torques matching is conducted.Meanwhile,a Nonlinear Model Predictive Control (NMPC) method is proposed,which combines the control index of the power turbine speed with torques matching of double engines creatively.In addition to the control index,the difference of output torques between each engine is also incorporated in the objective function as a penalty term to ensure constant speed control and short torques matching time.Simulation results demonstrate that relative to unilateral torques matching,the settling time of the bidirectional matching method can be reduced by nearly 30.8%.Nevertheless,compared with the bidirectional torques matching method under the cascade PID controller,the NMPC method can decrease the overshoot of the power turbine speed by 65%and reduce the matching time by 15.5%synchronously.Besides fast response control of turboshaft engines,fast torques matching control of double engines is accomplished as well.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2020年第2期561-571,共11页 中国航空学报(英文版)
基金 co-supported by the National Natural Science Foundation of China(No.51576096) Qing Lan and 333 Project and Research Funds for Central Universities(No.NF2018003).
关键词 DOUBLE turboshaft engines Fast response CONTROL HELICOPTER Nonlinear model PREDICTIVE CONTROL TORQUES MATCHING method Double turboshaft engines Fast response control Helicopter Nonlinear model predictive control Torques matching method
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