Optimized Model Predictive Control for Unmanned Aerial Vehicles with Sensor Uncertainties

A. Azar, Fernando E. Serrano, Nashwa Ahmad Kamal, B. Qureshi, Ammar K. Al Mhdawi, A. Humaidi, I. Ibraheem, Chakib Ben Njima
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引用次数: 2

Abstract

In this paper, a novel control strategy based on model predictive control is proposed for tracking the trajectory of unmanned aerial vehicles (UAV). First, the dynamic model of an unmanned aerial vehicle UAV is established by considering the linear velocities in terms of the analyzed system’s attitude angles. The UAV’s dynamic model is suitable for kinematic control by using two attitude angles as control inputs. The controller design is made up of an output feedback controller formed by the error variables, which are the difference between the measured output and the reference variables. Then, a model predictive control is established by considering an optimization problem with a performance index and the corresponding constraints. Furthermore, the stochastic properties of the UAV dynamic model are taken into account in this research study. The measured outputs provided by the sensors are constrained by the topological characteristics of the unmanned aerial vehicle to be analyzed. Finally, a numerical experiment and its conclusions are presented, demonstrating that the proposed control strategy provides optimal trajectory tracking.
具有传感器不确定性的无人机优化模型预测控制
提出了一种基于模型预测控制的无人机轨迹跟踪控制策略。首先,根据所分析系统的姿态角考虑线速度,建立了无人机的动力学模型;采用两个姿态角作为控制输入,无人机的动力学模型适合于运动学控制。控制器设计由误差变量组成的输出反馈控制器组成,误差变量是测量输出与参考变量的差值。然后,考虑具有性能指标和约束条件的优化问题,建立模型预测控制。此外,本文还考虑了无人机动力学模型的随机特性。传感器提供的测量输出受待分析无人机拓扑特性的约束。最后,给出了一个数值实验和结论,证明了所提出的控制策略能够实现最优的轨迹跟踪。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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