Fixed-time disturbance observer-based robust fault-tolerant tracking control for uncertain quadrotor UAV subject to input delay

This study focuses on the design of a fixed-time disturbance observer-based robust fault-tolerant tracking control scheme for an uncertain quadrotor unmanned aerial vehicle (UAV), which allows the quadrotor UAV to track a presupposed trajectory despite the simultaneous existence of model uncertainti...

Celý popis

Uloženo v:
Podrobná bibliografie
Vydáno v:Nonlinear dynamics Ročník 107; číslo 3; s. 2363 - 2390
Hlavní autoři: Liu, Kang, Wang, Rujing, Zheng, Shijian, Dong, Shifeng, Sun, Guowei
Médium: Journal Article
Jazyk:angličtina
Vydáno: Dordrecht Springer Netherlands 01.02.2022
Springer Nature B.V
Témata:
ISSN:0924-090X, 1573-269X
On-line přístup:Získat plný text
Tagy: Přidat tag
Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!
Popis
Shrnutí:This study focuses on the design of a fixed-time disturbance observer-based robust fault-tolerant tracking control scheme for an uncertain quadrotor unmanned aerial vehicle (UAV), which allows the quadrotor UAV to track a presupposed trajectory despite the simultaneous existence of model uncertainties, external disturbances, actuator faults, and input delay. First of all, the combination of Pade approximation and an intermediate variable is employed to reduce the complexity of studying the quadrotor system with input delay. Secondly, the fixed-time disturbance observer is proposed to eliminate the effects of the composite disturbances without requiring some serious assumptions. Subsequently, the new nonsingular fixed-time sliding mode manifold and the auxiliary system are developed to overcome the singular problem without any piecewise continuous functions. In the sense of the Lyapunov theorem, it is proved that the tracking errors of the closed-loop system converge to the origin within a fixed time regardless of the initial conditions. Eventually, extensive comparative simulations are performed to manifest the feasibility and validity of the proposed control strategy in terms of disturbance rejection, fault-tolerance, chattering elimination, and singularity-free.
Bibliografie:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:0924-090X
1573-269X
DOI:10.1007/s11071-021-07080-0