4.4 Article

Prescribed performance-based tracking control for quadrotor UAV under input delays and input saturations

Journal

Publisher

SAGE PUBLICATIONS LTD
DOI: 10.1177/01423312211067291

Keywords

Disturbed quadrotor UAV; input delays; input saturations; prescribed performance; semi-globally UUB

Funding

  1. National Science Fund for Distinguished Young Scholars [61825302]
  2. National Natural Science Foundation of China [U2013201]
  3. Key R&D projects (Social Development) in Jiangsu Province of China [BE2020704]

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In this paper, a semi-global trajectory tracking control scheme is proposed for quadrotor UAV with time-varying input delays, input saturations, and bounded disturbances. By introducing error transformation function, state prediction method, and dynamic surface control, the proposed scheme can limit the tracking error within the prescribed bound and ensure that all signals in the closed-loop system are bounded.
In this paper, a semi-global trajectory tracking control scheme is proposed for quadrotor unmanned aerial vehicle (UAV) under time-varying input delays, input saturations, and bounded disturbances. Initially, in order to ensure the desirable control performance that tracking error is limited in a prescribed bound, an error transformation function is presented to transform the constrained problem into a stabilization one. Then, under backstepping control scheme, a state prediction method combined with a dynamic surface control (DSC) is presented to compensate for the effects of input delays, and an auxiliary system is designed to tackle the input saturations, which are further to deal with input delays and input saturations in both position system and attitude system of quadrotor UAV. Particularly, the Euler angle is constrained to avoid the singular points of the attitude system. Besides, based on Lyapunov stability theory, it can be verified that all signals in the closed-loop system of the quadrotor UAV are semi-globally ultimately uniformly bounded (UUB) and the tracking errors are restrained in the prescribed bounds. Finally, by choosing some appropriate parameters, the simulation results based on quadrotor UAV model are given to verify the effectiveness of the proposed control scheme.

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