An experimental analysis of a robust event triggered super twisting sliding mode control for Quadcopter trajectory tracking

Sarika Raju, Ezhilarasi Deenadayalan, Ramakalyan Ayyagari
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Abstract

An event-triggered-super twisting sliding mode control (ET-STSMC) with saturation function in reaching law have been designed for a nonlinear Quadcopter model with bounded disturbance and its performance is compared with Event Triggered-Sliding mode control (ET-SMC). Simulation results have been obtained for altitude and attitude tracking, demonstrating the stability of the closed-loop system with the proposed control. The event-triggering conditions are derived based on the Lyapunov method, ensuring non-accumulation of inter-event execution time. Experiments have been performed in real-time to analyse the robustness and computational cost in terms of the number of control updates of the proposed control strategy under normal flight, external disturbances, and parameter uncertainty. Simulation and experimental results show that ET-STSMC can achieves better tracking performance and robustness with reduced computational cost compared to ET-SMC during all flight conditions.

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用于四旋翼飞行器轨迹跟踪的鲁棒事件触发超扭曲滑模控制实验分析
针对具有有界干扰的非线性四旋翼飞行器模型,设计了一种带有饱和函数的事件触发超扭曲滑模控制(ET-STSMC),并将其性能与事件触发滑模控制(ET-SMC)进行了比较。获得了高度和姿态跟踪的仿真结果,证明了采用所提议的控制方法的闭环系统的稳定性。基于 Lyapunov 方法得出了事件触发条件,确保事件间执行时间不会累积。在正常飞行、外部干扰和参数不确定的情况下,进行了实时实验,分析了所提控制策略的鲁棒性和控制更新次数方面的计算成本。仿真和实验结果表明,与 ET-SMC 相比,ET-STSMC 在所有飞行条件下都能实现更好的跟踪性能和鲁棒性,并降低了计算成本。
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