对数线性动态反演控制在多旋翼机上的应用

Li-Yu Lin, James Goppert, Inseok Hwang
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引用次数: 0

摘要

本文提出了一种方法,利用李群理论中的对数线性化和牛顿-欧拉方程,推导出多旋翼模型的精确线性误差动态,并将该模型与新型对数线性动态反转控制器相结合,以简化非线性失真并增强对数线性化系统的稳健性。此外,我们还利用线性矩阵不等式(Linear MatrixInequalities,LMI)来约束对数线性化在有界干扰输入情况下的跟踪误差,并利用指数图计算非线性系统在李群中的不变集。我们通过一个有参考轨迹的多旋翼系统示例演示了我们方法的有效性,结果验证了在有界扰动情况下跟踪误差的安全保证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Application of Log-Linear Dynamic Inversion Control to a Multi-rotor
This paper presents an approach that employs log-linearization in Lie group theory and the Newton-Euler equations to derive exact linear error dynamics for a multi-rotor model, and applies this model with a novel log-linear dynamic inversion controller to simplify the nonlinear distortion and enhance the robustness of the log-linearized system. In addition, we utilize Linear Matrix Inequalities (LMIs) to bound the tracking error for the log-linearization in the presence of bounded disturbance input and use the exponential map to compute the invariant set of the nonlinear system in the Lie group. We demonstrate the effectiveness of our method via an illustrative example of a multi-rotor system with a reference trajectory, and the result validates the safety guarantees of the tracking error in the presence of bounded disturbance.
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