自主导航的观察者控制方案:四旋翼飞行器的飞行试验验证

L. E. Munoz, P. Castillo, P. Garcia
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引用次数: 14

摘要

本文提出了一种基于李雅普诺夫分析和饱和函数的非线性控制算法的改进,以实现四旋翼飞行器的自主导航。对算法进行了分析,改善了状态的收敛性,并利用这些新条件证明了闭环系统的稳定性分析。为了对飞行器进行定位,提出了一种基于扩展卡尔曼滤波的航位推算算法。该算法基于传统传感器的数据融合;惯性测量单元(IMU)、超声波传感器和视觉系统。通过飞行试验验证了算法的有效性,实现了四旋翼飞行器的自主导航。一些图表描述了最重要的结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Observer-control scheme for autonomous navigation: Flight tests validation in a quadrotor vehicle
We present in this paper an improvement of a nonlinear control algorithm based on the Lyapunov analysis and the saturation functions, to realize autonomous navigation of a quadrotor vehicle. The algorithm is analyzed and the convergence of the states is ameliorated, in addition, the stability analysis in closed-loop system is proved with these new conditions. In order to locate the aerial vehicle a new position estimation algorithm is developed using the dead-reckoning technique with the Extended Kalman Filter (EKF). This algorithm is based in the data fusion of the classical sensors; an Inertial Measurement Unit (IMU), an ultrasonic sensor and a vision system. The algorithms are validated onboard in flight tests to realize autonomous navigation of the quadrotor vehicle. The most important results are depicted in some graphs.
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