Adaptive dynamic programming base on MMC device of a flexible high-altitude long endurance aircraft

• Published in: Aerospace science and technology Vol. 151; p. 109305
• Main Authors: Yuan, LaoHu, Wang, LiDong, Zhang, JinXiu
• Format: Journal Article
• Language: English
• Published: Elsevier Masson SAS 01.08.2024
• Subjects: Adaptive dynamic programming; Attitude control; Disturbance observer; Flexible aircraft; Moving-mass control; Moving-mass control; Disturbance observer; Attitude control; Adaptive dynamic programming; Flexible aircraft
• ISSN: 1270-9638; 1626-3219
• DOI: 10.1016/j.ast.2024.109305

Flexible high-altitude long endurance (HALE) aircraft face challenges such as the delay effect caused by aeroelasticity and low efficiency during high-altitude cruising. This paper addresses a new active control scheme that replaces traditional aerodynamic control surfaces with longitudinal and lateral moving masses and adopts an observer-based adaptive dynamic programming (ADP) control strategy, aiming to solve the attitude control of HALE aircraft with flexible wings. Firstly, considering the account of unsteady aerodynamics, attitude angular velocity, and moving masses, complete dynamic model is established for a flexible aircraft, in order to more accurately describe the state of the HALE aircraft. This model includes two moving masses to replace traditional ailerons and elevators. It is difficult to design attitude control strategies considering the delay effects and unknown dynamic disturbances of HALE aircraft. To this end, the actor-critic structure of the ADP approach is designed to achieve the near-optimal control strategy of the system, which eliminates the need for prior knowledge of model parameters. A fixed time disturbance observer (FTDO) is proposed to estimate the future tracking error information and unknown disturbances to improve the control performance of the attitude. Finally, the stability of the system is proved via the Lyapunov technique and a comprehensive simulation of HALE aircraft is provided. The simulation results show that the proposed control algorithm can enable the aircraft attitude angles to quickly response and maintain stability under gust wind. Compared with a single ADP control strategy, this paper's algorithm has advantages in response speed and error.