Modeling and Simulation Based Turboprop Engine Control Technology

摘要：

A type of turboprop engine acceleration features and regulation analysis based on a core engine model was carried out. The combination of core engine model and fuel-propeller integrated mechanism was detailed. Fuel-propeller integrated model was built up for further Proportional Integral Differential (PID) controller design. Based on the integrated model, a close-loop controller engine was designed. A feedforward section was added to the system for engine power overshoot constraint Simulation validation was evaluated and verified by comparing the experimental rig test data and simulation output data.

关键词： turboprop modeling simulation feedforward acceleration model validation overshoot

作者: TIAN Chao HUANG Xiang-hua DENG Zhi-wei

作者单位: College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing, Aviation Motor Control System Institute, Aviation Industry Corporation of China,Wuxi, P.R.China

会议类型: 国际会议

会议名称: The 3rd International Symposium on Jet Propulsion and Power Engineering(第三届喷气推进与动力工程国际会议 ISJPPE)

会议地点: 南京

会议语种:英文

页码: 583-588

在线出版日期: 2010-09-13（万方平台首次上网日期，不代表论文的发表时间）