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具有定量超調約束的四旋翼無人機預設性能控制

Pre-performance control for quadrotor UAV with quantitative overshoot constraints

  • 摘要: 針對具有時變擾動的四旋翼無人機的超調定量約束問題,提出了一種基于新型時變障礙Lyapunov函數的預設性能神經網絡自適應控制方法。首先,對四旋翼無人機的超調約束問題進行分析,針對超調約束問題,提出一種新型時變障礙Lyapunov函數,所提出的新型時變障礙Lyapunov函數能夠對系統施加連續的非對稱約束,從而更精細的約束系統的行為,豐富了預設性能邊界的設置形式。其次,設計新型的管狀預設性能邊界函數,進而對系統輸出的超調量施加定量約束,并且滿足穩態性能要求。在此基礎上,通過反演法設計反饋控制律和神經網絡自適應律,保證系統的性能約束。最后,基于Lyapunov函數穩定性理論證明所有閉環信號的一致最終有界性,并通過數值仿真進行實驗對比,對所提出方法的有效性進行驗證。仿真結果表明,所提出的控制律能夠實現對于四旋翼無人機超調的定量約束。

     

    Abstract: Aiming at the overshoot quantitative constraint problem of quadrotor UAV with time-varying disturbance, a neural network adaptive control method with preset performance based on a new Lyapunov function with time-varying obstacles was proposed. Firstly, the overshoot constraint problem of the quadrotor UAV was analyzed, and a new time-varying barrier Lyapunov function was proposed for the overshoot constraint problem. The new time-varying barrier Lyapunov function can impose continuous asymmetric constraints on the system, so as to constrain the behavior of the system more accurately and enrich the setting form of the preset performance boundary. Secondly, a new tubular preset performance boundary function is designed to impose quantitative constraints on the overshoot of the system output and meet the steady-state performance requirements. On this basis, the feedback control law and the neural network adaptation law are designed by the backstepping method to ensure the performance constraints of the system. Finally, based on the Lyapunov function stability theory, the uniform ultimate boundedness of all closed-loop signals is proved, and the effectiveness of the proposed method is verified by numerical simulation. Simulation results show that the proposed control law can achieve quantitative constraints on the overshoot of the quadrotor UAV. Considering the realistic conditions and safety factors, such as when the UAV passes through a narrow passage and when the UAV is hanging to carry goods, it is often necessary to impose certain constraints on the overshoot of the system. In the current control methods, the transient performance of the system is generally adjusted by adjusting the parameters, although there are many studies on adjusting the overshoot of the system. However, none of these studies can achieve a quantitative constraint on the overshoot. Therefore, in this paper, we focus on the quantitative constraint problem of the overshoot of the quadrotor UAV from the basic viewpoint of constraint control. Firstly, a barrier Lyapunov function is designed, which does not depend on the switching function and can impose continuous asymmetric constraints on the system. Then, a new tubular preset performance boundary function is designed based on the asymmetric barrier Lyapunov function, which can predefine a more accurate and flexible tubular working region. Moreover, the system position error is limited to the working region, and then the overshoot of the system is quantitatively constrained. Secondly, the neural network adaptive control technology is introduced, the RBF neural network is selected as the observer of the system, and its adaptive law is designed to estimate the multi-source time-varying disturbance of the UAV. The simulation verification is carried out by setting up the comparison experiment of two scenarios. The results show that the system error can be constrained in the predefined tubular working area, and the proposed control strategy can quantitatively constrain the overshoot of the quadrotor UAV system, and has high steady-state accuracy and robustness. Compared with other traditional control methods, the proposed control strategy can reduce the overshoot of the quadrotor UAV system. The control method proposed in this paper can design the transient and steady-state performance of the system in advance without adjusting the parameters.

     

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