多工况下四旋翼飞行器系统特性与自适应跟踪控制

Yu Sheng, G. Tao
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引用次数: 2

摘要

本文提出了一种四旋翼系统输入补偿自适应控制器设计框架,该框架以统一的控制器参数更新规律处理不同的系统运行条件。研究的目的是为了解决现有的自适应控制方案以系统平衡状态为悬停条件或无法处理引起系统交互器矩阵和高频增益矩阵变化的各种系统不确定性的问题。构造了一种带输入补偿器的自适应控制方案,使系统在不同工况下具有均匀的交互器矩阵和一致的增益矩阵符号模式,这是模型参考自适应控制应用于四旋翼系统的关键先验设计条件。针对系统高频增益矩阵的不确定性,采用增益矩阵分解技术,根据增益参数和跟踪误差对误差系统模型进行参数化,设计了系统知识减少的自适应参数更新律。该方法保证了闭环系统的所有信号都是有界的,并且在非平衡运行条件下,尽管存在系统参数的不确定性和不确定的偏移量,系统输出仍能渐近地跟踪参考输出。该方案扩展了四旋翼机在存在系统不确定性的多种工况下的自适应控制能力。最后给出了采用该自适应控制方案的四旋翼飞行器的仿真结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
System Characterization and Adaptive Tracking Control of Quadrotors under Multiple Operating Conditions
This paper presents an adaptive controller design framework with input compensation for quadrotor systems, which deals with different system operating conditions with a uniform update law for the controller parameters. The motivation of the work is to handle the situation that existing adaptive control schemes are either restricted to the system equilibrium as the hover condition or unable to deal with the diverse system uncertainties which cause system interactor matrix and high-frequency gain matrix to change. An adaptive control scheme equipped with an input compensator is constructed to make the system to have a uniform interactor matrix and a consistent pattern of the gain matrix signs over different operating conditions, which are key prior design conditions for model reference adaptive control applied to quadrotor systems. To deal with the uncertain system high-frequency gain matrix, a gain matrix decomposition technique is employed to parametrize an error system model in terms of the gain parameters and tracking errors, for the design of an adaptive parameter update law with reduced system knowledge. It is ensured that all closed-loop system signals are bounded, and the system output tracks a reference output asymptotically despite the system parameter uncertainties and the uncertain offsets at non-equilibrium operating conditions. The proposed scheme expands the capacity of adaptive control for quadrotors to operate at multiple operating conditions in the presence of system uncertainties. Simulation results of a quadrotor with the proposed adaptive control scheme are presented to show the desired system performance.
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