TY - GEN
T1 - Novel control strategy for balancing resources and performance of constrained flexible hypersonic vehicles
AU - Zhao, Tianlong
AU - Hao, Fei
N1 - Publisher Copyright:
© 2024 Technical Committee on Control Theory, Chinese Association of Automation.
PY - 2024
Y1 - 2024
N2 - This article aims to derive an anti-disturbance tracking control algorithm for flexible air-breathing hypersonic vehicles (FAHVs) with uncertain aerodynamic parameters, external disturbances, input saturation and limited transmission resources. Based on the framework of the backstepping technique, a novel event-triggered appointed-time fast tracking control protocol is proposed. Firstly, augmented sliding mode observers are used to provide the estimation of the lumped disturbances. Then, to guarantee satisfactory transient response and steady-state performance, the practical fixed-time controller and the appointedtime prescribed performance controller are designed. In addition, to address the problem of actuator saturation, the auxiliary system and the saturation approximate function are introduced. Finally, two event-triggered mechanisms are applied to exactly determine when control signals should be updated, which naturally eliminate unnecessary waste of transmission resources. Our proposed method not only reduces the execution frequency of the actuator, but also further optimizes the transient and steady-state performance. The proposed control scheme achieves a balance between reducing communication frequency and improving the closed-loop system performance. The feasibility and the effectiveness of the proposed strategy is validate through simulations.
AB - This article aims to derive an anti-disturbance tracking control algorithm for flexible air-breathing hypersonic vehicles (FAHVs) with uncertain aerodynamic parameters, external disturbances, input saturation and limited transmission resources. Based on the framework of the backstepping technique, a novel event-triggered appointed-time fast tracking control protocol is proposed. Firstly, augmented sliding mode observers are used to provide the estimation of the lumped disturbances. Then, to guarantee satisfactory transient response and steady-state performance, the practical fixed-time controller and the appointedtime prescribed performance controller are designed. In addition, to address the problem of actuator saturation, the auxiliary system and the saturation approximate function are introduced. Finally, two event-triggered mechanisms are applied to exactly determine when control signals should be updated, which naturally eliminate unnecessary waste of transmission resources. Our proposed method not only reduces the execution frequency of the actuator, but also further optimizes the transient and steady-state performance. The proposed control scheme achieves a balance between reducing communication frequency and improving the closed-loop system performance. The feasibility and the effectiveness of the proposed strategy is validate through simulations.
KW - Hypersonic vehicle
KW - appointed-time control
KW - constraints
KW - event-triggered control
KW - practical fixed-time control
UR - https://www.scopus.com/pages/publications/85205491320
U2 - 10.23919/CCC63176.2024.10662005
DO - 10.23919/CCC63176.2024.10662005
M3 - 会议稿件
AN - SCOPUS:85205491320
T3 - Chinese Control Conference, CCC
SP - 622
EP - 627
BT - Proceedings of the 43rd Chinese Control Conference, CCC 2024
A2 - Na, Jing
A2 - Sun, Jian
PB - IEEE Computer Society
T2 - 43rd Chinese Control Conference, CCC 2024
Y2 - 28 July 2024 through 31 July 2024
ER -