四旋翼系统的速率控制和飞行稳定

Benjamin Jahn, Alexander Barth, K. Wulff, Tobias Simon, Jan Romisch
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引用次数: 5

摘要

在本文中,我们提出了一个四旋翼飞机的稳定性增强系统,使人类飞行员能够直接控制速度。我们的系统包括用于速率控制的前馈,用于干扰衰减的反馈,以及用于处理输入限制的在线优化技术。我们证明了所提出的算法能够在极具挑战性的飞行条件下稳定系统,例如阵风和快速手动下降。我们的输入限制技术保证了所需转矩的转速是可行的。利用MATLAB对整个控制系统进行了分析,并基于四旋翼样机进行了充分的实验验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Rate control and flight stabilization for a quadrotor system
In this paper we propose a stability augmentation system for a quadrotor, enabling direct rate control for a human pilot. Our system includes feedforward for rate control, feedback for disturbance attenuation, and an online optimization technique for handling input restrictions. We show that the proposed algorithms are able to stabilize the system under highly challenging flight conditions, such as wind gusts and fast manual descend. Our input restriction technique ensures that the revolution speeds for the desired torques are feasible. The complete control system is analyzed using MATLAB, and full experimental validation is provided based on a quadrotor prototype.
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