Quadrotor Fault-Tolerant Constrained Control Using Interval Contractor-Based Adaptive Reference Governor

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-09-10 DOI:10.1109/TAES.2024.3456749
Guido Magnani;Mario Cassaro;Jean-Marc Biannic;Hélène Evain;Laurent Burlion
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Abstract

This article proposes a solution to handle the propeller failure on a quadrotor subject to state and input constraints. A model reference adaptive control law compensates for the fault and the unmodeled quadrotor dynamics, while a robust reference governor (RG) enforces state and input constraints. Differently from existing works, the governor is built in accordance with the adaptive control law performance guarantees and adapts its propagation model online as soon as a contraction algorithm detects the fault. As shown in the numerical simulation, the solution allows both precise reference tracking and constraint enforcement at the price of reduced conservatism with respect to the usual robust RG scheme.
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利用基于时间间隔承包商的自适应参考调速器实现四旋翼飞行器容错约束控制
针对四旋翼飞行器在状态和输入约束下的螺旋桨失效问题,提出了一种解决方案。模型参考自适应控制律补偿故障和未建模的四旋翼动力学,而鲁棒参考调节器(RG)执行状态和输入约束。与现有工作不同的是,该调速器是根据自适应控制律性能保证构建的,一旦收缩算法检测到故障,就在线调整其传播模型。如数值模拟所示,该解决方案允许精确的参考跟踪和约束执行,但代价是相对于通常的鲁棒RG方案降低了保守性。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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