TY - JOUR
T1 - Asymmetric error-constrained path-following control of a stratospheric airship with disturbances and actuator saturation
AU - Chen, Tian
AU - Zhu, Ming
AU - Zheng, Zewei
N1 - Publisher Copyright:
© 2018 Elsevier Ltd
PY - 2019/3/15
Y1 - 2019/3/15
N2 - This paper addresses the asymmetric error-constrained path-following problem of a stratospheric airship with external disturbances and actuator saturation. A path-following algorithm is proposed based on the theories of tan-type barrier Lyapunov function, vector field guidance, adaptive sliding mode control, and radial basis function neural network (RBFNN). First, to satisfy the asymmetric tracking error-constrained requirements of airship position, an asymmetric error-constrained vector field (AECVF) guidance law is presented, which can navigate the stratospheric airship along the predefined path and guarantee that the tracking error is limited by the error constraints. Second, an adaptive sliding mode attitude controller is introduced to track the desired attitudes calculated using the AECVF with disturbances. Finally, an adaptive velocity controller is added to the control algorithm to maintain an appropriate velocity. Moreover, an RBFNN saturation compensator is introduced to solve the actuator saturation problem caused by the low maneuverability. Stability analysis indicates that all the signals in the closed-loop system are uniformly ultimately bounded. Meanwhile, simulation results demonstrate the effectiveness of the proposed control algorithm.
AB - This paper addresses the asymmetric error-constrained path-following problem of a stratospheric airship with external disturbances and actuator saturation. A path-following algorithm is proposed based on the theories of tan-type barrier Lyapunov function, vector field guidance, adaptive sliding mode control, and radial basis function neural network (RBFNN). First, to satisfy the asymmetric tracking error-constrained requirements of airship position, an asymmetric error-constrained vector field (AECVF) guidance law is presented, which can navigate the stratospheric airship along the predefined path and guarantee that the tracking error is limited by the error constraints. Second, an adaptive sliding mode attitude controller is introduced to track the desired attitudes calculated using the AECVF with disturbances. Finally, an adaptive velocity controller is added to the control algorithm to maintain an appropriate velocity. Moreover, an RBFNN saturation compensator is introduced to solve the actuator saturation problem caused by the low maneuverability. Stability analysis indicates that all the signals in the closed-loop system are uniformly ultimately bounded. Meanwhile, simulation results demonstrate the effectiveness of the proposed control algorithm.
KW - Asymmetric error constraints
KW - Path following control
KW - Stratospheric airship
KW - Vector field
UR - https://www.scopus.com/pages/publications/85054877651
U2 - 10.1016/j.ymssp.2018.10.003
DO - 10.1016/j.ymssp.2018.10.003
M3 - 文章
AN - SCOPUS:85054877651
SN - 0888-3270
VL - 119
SP - 501
EP - 522
JO - Mechanical Systems and Signal Processing
JF - Mechanical Systems and Signal Processing
ER -