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

• Published in: International journal of robust and nonlinear control 2019-11, Vol.29 (16), p.5820-5844
• Main Authors: Emami, Seyyed Ali, Banazadeh, Afshin
• Format: Article
• Language: English
• Subjects: actuator faults; Actuators; Aerodynamics; Aircraft; Aircraft control; Algorithms; Computer simulation; disturbance observer‐based model predictive control (DOb‐MPC); Disturbances; Dynamic stability; Faults; flight control systems; Iterative methods; Machine learning; Neural networks; nonlinear autoregressive with eXogenous input (NARX) neural network; OS‐MMS; Predictive control; Structural damage; Tracking control; Trajectory control; trajectory tracking; Turbulence
• ISSN: 1049-8923; 1099-1239
• DOI: 10.1002/rnc.4698

Summary 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.