基于增量动态逆的大型民用飞机容错控制策略  

Fault Tolerant Strategy for a Large Civil Aircraft Based on Incremental Nonlinear Dynamic Inversion

作　　者：秦天成 刘世前[1] 桑元俊 王旭东 QIN Tian-cheng;LIU Shi-qian;SANG Yuan-jun;WANG Xu-dong(School of Aeronautics and Astronautics,Shanghai Jiao Tong University,Shanghai 200240,China)

机构地区：[1]上海交通大学航空航天学院,上海200240

出　　处：《科学技术与工程》2021年第2期839-844,共6页Science Technology and Engineering

基　　金：工业和信息化部民用飞机专项(MJZ-2016-S-04)。

摘　　要：作动器故障是大型民用飞机飞行安全中面临的重要难题,为此,提出一种增量动态逆的容错控制方法,来解决飞行控制系统故障模式下的安全飞行控制问题。首先建立大型民用飞机非线性动力学模型及执行器故障模型;其次,根据非线性动态逆理论,提出增量形式的动态逆算法,并针对执行器故障模式,设计相应的容错控制器,增量动态逆控制引入加速度信号反馈,降低了控制律对于模型的敏感度,提高了闭环系统的鲁棒性。针对姿态回路跟踪,设计了增量动态逆姿态控制器。最后,以某型民用飞机为对象,开展了执行器故障模式下姿态角跟踪控制仿真。仿真结果显示,增量动态逆控制律在大型民用飞机的容错控制策略方案中克服了模型的不确定性,且可以达到较好的控制效果。Actuator fault is an important problem in the flight safety of large civil aircraft.Therefore,a fault-tolerant control strategy with nonlinear incremental dynamic inversion method was proposed to deal with actuator faults generated during the flight process.Firstly,the nonlinear dynamic model and actuator fault model of large civil aircraft were established.Secondly,according to the nonlinear dynamic inversion theory,an incremental dynamic inversion algorithm was proposed,and the corresponding fault-tolerant controller was designed for the actuator fault model;the algorithm used acceleration signal as feedback,which reduced the model sensitivity to the model and improved the robustness of the closed-loop system.An nonlinear incremental dynamic inversion attitude controller was designed for attitude loop tracking.Finally,with a certain type of civil aircraft as the object,the simulation of the attitude angle tracking control in the actuator fault mode was carried out to verify the feasibility of the nonlinear incremental dynamic inversion fault-tolerant control method.

关 键 词：非线性动态逆 增量动态逆 容错控制 作动器故障 

分 类 号：V249.12[航空宇航科学与技术—飞行器设计]