An adaptive recursive sliding mode attitude control for tiltrotor UAV in flight mode transition based on super-twisting extended state observer
Mengshan Xie, Sheng Xu, Cheng-yue Su, Zu-yong Feng, Yuandian Chen,, Zhenhua Shi, Jiebo Lian

TL;DR
This paper presents an adaptive recursive sliding mode control method combined with a super-twisting extended state observer for tiltrotor UAVs, improving attitude control during flight mode transitions by enhancing disturbance rejection.
Contribution
It introduces a novel STESO-ARSMC control scheme that integrates state estimation and adaptive control for tiltrotor UAVs, addressing nonlinearities and disturbances during transition modes.
Findings
Enhanced anti-disturbance performance demonstrated in simulations
Finite-time convergence of the control system achieved
Effective attitude control during flight mode transition
Abstract
With the characteristics of vertical take-off and landing and long endurance, tiltrotor has attracted considerable attention in recent decades for its potential applications in civil and scientific research. However, the problems of strong couplings, nonlinear characteristics and mismatched disturbances inevitably exist in the tiltrotor, which bring great challenges to the controller design in transition mode. In this paper, we combined a super-twisting extended state observer (STESO) with an adaptive recursive sliding mode control (ARSMC) together to design a tiltrotor aircraft attitude system controller in transition mode using STESO-ARSMC (SAC). Firstly, the six degrees of freedom (DOF) nonlinear mathematical model of tiltrotor is established. Secondly, the states and disturbances are estimated by the STES observer. Thirdly, ARSM controller is designed to achieve finite time…
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Taxonomy
TopicsAdaptive Control of Nonlinear Systems · Control and Dynamics of Mobile Robots · Distributed Control Multi-Agent Systems
