Real-Time OF-based Trajectory Control of a UAS Rotorcraft Based on Integral Extended-State LQG

Tariq Zioud, J. Escareño, O. Labbani-Igbida
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Abstract

The actual paper proposes a robust optimal control strategy via an Extended-State Integral Linear Quadratic Gaussian (ES-iLQG) controller meant to drive the quadrotor motion to track a time-parametrized trajectory in presence of exogenous and endogenous disturbances. The herein enhanced LQG controller, includes an Extended-State Linear Kalman Filter (ES-LKF) utilised as a disturbance estimator, and an integral Linear Quadratic Regulator (iLQR). Results from a simulation stage exhibit the effectiveness of the proposed control scheme for trajectory tracking purposes. In this regard, promising experimental results were obtained from two scenarios: Trajectory tracking of an elliptical helix-shaped and an 8-shaped trajectories. It is noteworthy that the control law is computed onboard and relies on optical flow for translational motion control.
基于积分扩展状态LQG的UAS旋翼机实时轨迹控制
实际论文提出了一种鲁棒最优控制策略,通过扩展状态积分线性二次高斯(ES-iLQG)控制器驱动四旋翼运动在存在外源和内源干扰的情况下跟踪时间参数化轨迹。本文改进的LQG控制器包括一个用作干扰估计器的扩展状态线性卡尔曼滤波器(ES-LKF)和一个积分线性二次调节器(iLQR)。仿真结果表明了该控制方案在弹道跟踪方面的有效性。在椭圆螺旋形轨迹跟踪和8形轨迹跟踪两种情况下,均获得了较好的实验结果。值得注意的是,控制律是机载计算的,并依靠光流进行平移运动控制。
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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