• 所属单位：能源与动力学院
• 发表刊物：ARABIAN JOURNAL FOR SCIENCE AND ENGINEERING
• 关键字：Helicopter Engine Integrated model Autorotation Control
• 摘要：In order to improve the helicopter responsive ability during autorotation power recovery maneuvers, a new turbo-shaft engine control scheme is proposed in this paper. Using rotor flapping/lagging dynamics and an induced velocity model which is capable of capturing vortex ring characteristics, an integrated helicopter and engine model was developed to simulate autorotation process. By introducing a closed-loop with compressor guided vanes, a novel two-variable engine control law is devised using Linear Matrix Inequality Pole Placement method. This allows for a rapid adaptation of the helicopter to a large and fast needed torque variation required in autorotation power recovery. The transient performances and the robustness for the closed-loop helicopter-pilot system are validated for some examples appropriated to autorotation training procedure. Simulation results illustrate that, with this novel control law, the helicopter's ability to respond during autorotation is strongly enhanced when compared to traditional cases.
• ISSN号：2193-567X
• 是否译文：否
• 发表时间：2017-07-01
• 合写作者：Sun, Fengyong
• 第一作者：张海波
• 通讯作者：张海波