Adaptive path following control of a stratospheric airship with full-state constraint and actuator saturation

In this paper, the path following problem is addressed for a stratospheric airship subject to full-state constraint, input saturation and external disturbances. A novel full-state constrained path-following algorithm, which ensures that all states of the system remain in the predetermined intervals,...

Celý popis

Uloženo v:
Podrobná bibliografie
Vydáno v:Aerospace science and technology Ročník 95; s. 105457
Hlavní autoři: Chen, Tian, Zhu, Ming, Zheng, Zewei
Médium: Journal Article
Jazyk:angličtina
Vydáno: Elsevier Masson SAS 01.12.2019
Témata:
Full-state constraint
Path-following control
Stratospheric airship
Vector field guidance
Stratospheric airship
Path-following control
Full-state constraint
Vector field guidance
ISSN:1270-9638, 1626-3219
On-line přístup:Získat plný text
Tagy: Přidat tag
Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!
Popis
Shrnutí:In this paper, the path following problem is addressed for a stratospheric airship subject to full-state constraint, input saturation and external disturbances. A novel full-state constrained path-following algorithm, which ensures that all states of the system remain in the predetermined intervals, is proposed based on the theories of barrier Lyapunov function, vector field guidance, adaptive backstepping control and saturation compensator. Firstly, an error-constrained vector field (ECVF) guidance law is presented to handle the position tracking error, which can navigate the stratospheric airship along the predefined path and guarantee that the error is limited by the time-varying asymmetric constraints. Secondly, a state-constrained adaptive attitude controller is introduced to track the desired attitude calculated by the ECVF, in which a saturation compensator of virtual control law is employed to handle the problem of angular velocity constraint. Finally, a state-constrained adaptive velocity controller is designed to maintain an appropriate scheduled velocity. Furthermore, two auxiliary design systems are used to deal with the actuator saturation problem, and adaptive laws are developed for handling dynamic couplings and unknown disturbances. Stability analysis implies that all signals in the closed-loop system are uniformly ultimately bounded, and all path-following state constraint requirements are never violated. Meanwhile, the effectiveness of the proposed control algorithm is demonstrated by comparative simulation results.
ISSN:1270-9638
1626-3219
DOI:10.1016/j.ast.2019.105457