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用于四旋翼飞行器滚转和俯仰估计的二阶滑模算法的分析与设计。

Analysis and design of second-order sliding-mode algorithms for quadrotor roll and pitch estimation.

作者信息

Chang Jing, Cieslak Jérôme, Dávila Jorge, Zolghadri Ali, Zhou Jun

机构信息

Institute of Precision Guidance and Control, Northwestern Polytechnical University, 710072 Xi'an, China.

University of Bordeaux, IMS Laboratory, F-33400 Talence, France.

出版信息

ISA Trans. 2017 Nov;71(Pt 2):495-512. doi: 10.1016/j.isatra.2017.09.012. Epub 2017 Sep 29.

Abstract

The problem addressed in this paper is that of quadrotor roll and pitch estimation without any assumption about the knowledge of perturbation bounds when Inertial Measurement Units (IMU) data or position measurements are available. A Smooth Sliding Mode (SSM) algorithm is first designed to provide reliable estimation under a smooth disturbance assumption. This assumption is next relaxed with the second proposed Adaptive Sliding Mode (ASM) algorithm that deals with disturbances of unknown bounds. In addition, the analysis of the observers are extended to the case where measurements are corrupted by bias and noise. The gains of the proposed algorithms were deduced from the Lyapunov function. Furthermore, some useful guidelines are provided for the selection of the observer turning parameters. The performance of these two approaches is evaluated using a nonlinear simulation model and considering either accelerometer or position measurements. The simulation results demonstrate the benefits of the proposed solutions.

摘要

本文所解决的问题是,在可获取惯性测量单元(IMU)数据或位置测量值的情况下,在不假设扰动界限已知的条件下对四旋翼飞行器的横滚和俯仰进行估计。首先设计了一种平滑滑模(SSM)算法,以在平滑干扰假设下提供可靠估计。接下来,通过第二种提出的自适应滑模(ASM)算法放宽了该假设,该算法可处理未知界限的干扰。此外,将观测器的分析扩展到测量值受偏差和噪声影响的情况。所提算法的增益由李雅普诺夫函数推导得出。此外,还为观测器调整参数的选择提供了一些有用的指导方针。使用非线性仿真模型并考虑加速度计测量值或位置测量值来评估这两种方法的性能。仿真结果证明了所提解决方案的优势。

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