TY - JOUR
T1 - Adaptive event-triggered quantized attitude control for QUAV with appointed-time prescribed performance function
AU - Li, Jing
AU - Wang, Haochen
AU - Yang, Chen
N1 - Publisher Copyright:
© 2024 Elsevier Masson SAS
PY - 2024/3
Y1 - 2024/3
N2 - This study proposes an adaptive event-triggered (ET) quantized attitude control for quadrotor unmanned aerial vehicle (QUAV) with an appointed-time prescribed performance function (PPF). The appointed-time PPF is developed to enforce attitude convergence to preset transient and steady regions within an appointed time. Furthermore, the radial basis function neural network (RBFNN) is adopted to tackle the system uncertainties. The disturbance observer is employed to estimate the compound disturbance of the optimal approximation error of RBFNN and the unknown external disturbance. Additionally, to reduce the communication burden of QUAV, the control signal derived from the backstepping method is transmitted to the actuator at every ET time after being quantified by the quantizer. A switching threshold strategy is proposed in the ET mechanism and a logarithmic uniform hysteresis quantizer is developed, better ensuring the system performance. Finally, the theoretical analysis proves that the signal of the closed-loop system is uniformly ultimately bounded without Zeno behavior. The superiority of the proposed attitude control strategy for QUAV is demonstrated through simulation results.
AB - This study proposes an adaptive event-triggered (ET) quantized attitude control for quadrotor unmanned aerial vehicle (QUAV) with an appointed-time prescribed performance function (PPF). The appointed-time PPF is developed to enforce attitude convergence to preset transient and steady regions within an appointed time. Furthermore, the radial basis function neural network (RBFNN) is adopted to tackle the system uncertainties. The disturbance observer is employed to estimate the compound disturbance of the optimal approximation error of RBFNN and the unknown external disturbance. Additionally, to reduce the communication burden of QUAV, the control signal derived from the backstepping method is transmitted to the actuator at every ET time after being quantified by the quantizer. A switching threshold strategy is proposed in the ET mechanism and a logarithmic uniform hysteresis quantizer is developed, better ensuring the system performance. Finally, the theoretical analysis proves that the signal of the closed-loop system is uniformly ultimately bounded without Zeno behavior. The superiority of the proposed attitude control strategy for QUAV is demonstrated through simulation results.
KW - Attitude control
KW - Event-triggered (ET) mechanism
KW - Logarithmic uniform hysteresis quantizer
KW - Prescribed performance function (PPF)
KW - Quadrotor unmanned aerial vehicle (QUAV)
UR - https://www.scopus.com/pages/publications/85185565953
U2 - 10.1016/j.ast.2024.108967
DO - 10.1016/j.ast.2024.108967
M3 - 文章
AN - SCOPUS:85185565953
SN - 1270-9638
VL - 146
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 108967
ER -