具有不确定参数的固定翼无人机无模型控制方法

J. Barth, Jean-Philippe Condomines, J. Moschetta, C. Join, M. Fliess
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引用次数: 8

摘要

本文介绍了一种应用于固定翼无人机的创新无模型控制(MFC)体系结构的初步成果。MFC是一种专门用于建模知识较差的系统的算法。事实上,为无人机建立一个可靠且具有代表性的空气动力学模型的成本促使了这种控制器的使用。通过利用纯数值模型,该算法提供了一种直观的方法来调整控制回路,而不需要任何关于被控系统的信息。我们建议将MFC架构扩展到固定翼无人机的情况下,研究不确定参数下的MFC特性。作为第一个结果,我们设计的MFC架构提供了一个连续的控制器,能够稳定两个不同的固定翼无人机的整个飞行包线。这些结果显示了有希望的自适应前景,并证明了MFC对不确定参数和干扰抑制都具有鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Model-Free Control Approach for Fixed-Wing UAVs with Uncertain Parameters Analysis
This paper presents first results of an innovative Model-Free Control (MFC) architecture applied to fixed-wing UAVs. MFC is an algorithm dedicated to systems with poor modeling knowledge. Indeed, the costs to derive a reliable and representative aerodynamic model for UAVs motivated the use of such a controller. By exploiting a purely numerical model, this algorithm provides an intuitive method to tune the control loop without any information about the controlled system. We propose to extend the MFC architecture to the case of fixed-wing UAVs and study the MFC properties in terms of uncertain parameters. As a first result, our designed MFC architecture provides a continuous controller able to stabilize the entire flight envelope of two different fixed-wing UAVs. These results show promising adaptive perspectives and demonstrate that MFC presents robust properties for both uncertain parameters and disturbance rejection.
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