四旋翼机指挥性能系统的改进

2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP) Pub Date : 2015-12-03 DOI:10.1109/SCP.2015.7342220

S. Zavadskiy, Daria Sharovatova

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引用次数: 2

摘要

研究了四旋翼飞行器的飞行控制问题。采用四自由度系统作为控制对象的模型。该系统的相态是沿垂直轴方向的加速度和欧拉角角速度。直升机的执行系统通过增加过滤器得到了改进。给出了带滤波器系统的阶跃响应。介绍了采用简单PI调节器和设计动态滤波器的质量绩效管理系统。

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Improvement of quadrocopter command performance system

It is considered the problem of quadrocopter flight control. A system with four degrees of freedom is used as a model of the control object. Phase states of this system are acceleration along the vertical axis and Euler angles angular rate. Copter's cxecutive system is improved by the addition of a filter. The step response of the system with filter is presented. Quality performance management system with simple PI regulator and with designed dynamic filter is demonstrated.

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2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP)

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