空军工程大学学报2024，Vol.25Issue(2)：21-31,11.DOI:10.3969/j.issn.2097-1915.2024.02.003
考虑推力陷阱的组合动力飞行器切换控制方法研究
A Switching Control Methodology for Hybrid Propulsion Aircraft in Consideration of Transition Thrust Pinch
摘要
Abstract
In view of the issue of transition thrust pinch during power transitions in hybrid propulsion air-craft,a switching control method is proposed for hybrid propulsion aircraft considering thrust pinch.Firstly,for the normal flight control requirements of hybrid propulsion aircraft,a normal flight controller is designed by using a sliding mode control approach based on the super-twisting algorithm,enabling the aircraft to achieve finite-time stable tracking of reference commands in the presence of disturbances.Sec-ondly,in consideration of the control constraints imposed by thrust losses during power transitions,an in-put-constrained controller is designed to facilitate limited-time convergence of tracking errors during the mode transition phase while reducing the demand for thrust.Furthermore,in combination with the con-trollers for a normal flight or on a mode transition phase,a soft switching control strategy for combined engine transitions is designed.Finally,the simulation experiments show that the designed controller can not only effectively avoid thrust loss phenomenon,and effectively ensure the stability and the robustness in the switching control system.关键词
组合动力飞行器/推力陷阱/切换控制/输入约束控制Key words
hybrid propulsion aircraft/transition thrust pinch/switching control/input constraint control分类
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张秀云,李梦龙,田栢苓,李智禹,宗群..考虑推力陷阱的组合动力飞行器切换控制方法研究[J].空军工程大学学报,2024,25(2):21-31,11.基金项目
国家自然科学基金(62273249,62373268,62373273,62073234,62022060,62103417) （62273249,62373268,62373273,62073234,62022060,62103417）
