Intelligent trajectory tracking of an aircraft in the presence of internal and external disturbances

被引:18
作者
Emami, Seyyed Ali [1 ]
Banazadeh, Afshin [1 ]
机构
[1] Sharif Univ Technol, Dept Aerosp Engn, Tehran 1136511155, Iran
关键词
actuator faults; disturbance observer-based model predictive control (DOb-MPC); flight control systems; nonlinear autoregressive with eXogenous input (NARX) neural network; OS-MMS; trajectory tracking; FAULT-TOLERANT CONTROL; MODEL-PREDICTIVE CONTROL; NONLINEAR-SYSTEMS; ADAPTIVE-CONTROL; IDENTIFICATION; UNCERTAINTY; PARAMETER; DYNAMICS;
D O I
10.1002/rnc.4698
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This research deals with developing an intelligent trajectory tracking control approach for an aircraft in the presence of internal and external disturbances. Internal disturbances including actuators faults, unmodeled dynamics, and model uncertainties as well as the external disturbances such as wind turbulence significantly affect the performance of the common trajectory tracking control approaches. There are several fault-tolerant control approaches in the literature to overcome the effects of specific actuator or sensor faults during the flight. However, trajectory tracking control of an air vehicle in the presence of unexpected faults and simultaneous presence of wind turbulence is still a challenging problem. In this paper, an intelligent neural network-based model predictive control structure is proposed, where the prediction model is updated in each iteration based on a novel proposed online sequential multimodel structure. A hybrid offline-online learning algorithm is adopted in the introduced online sequential multimodel structure to identify the time-varying dynamics of the system. The proposed control structure can satisfactorily deal with unexpected actuator faults and structural damages as well as unmodeled dynamics and wind turbulence. The stability of the closed-loop system is proved under some realistic assumptions. The simulation results demonstrate the high capability of the proposed approach for trajectory tracking control of a conventional aircraft in the simultaneous presence of system faults and external disturbances.
引用
收藏
页码:5820 / 5844
页数:25
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