采用增益调度和PID控制器的自调平直升机的设计与构造

Ian Jannasch, D. Sabatta
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引用次数: 2

摘要

提出了一种倾转旋翼直升机的控制系统。这种飞行器有3组螺旋桨,其中一组安装在伺服上控制偏航运动。这导致了不对称,这就需要一个更复杂的控制系统来实现稳定。本文提出了一种针对该型直升机的增益调度PID控制系统。通过对俯仰和横摇的正负偏移使用解耦控制系统,以及对偏航使用单独的控制器来实现飞行稳定性。我们给出了这些控制器的阶跃响应,并表明所提出的系统能够使直升机在飞行中稳定
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and construction of a self-levelling tricopter using gain scheduling and PID controllers
This paper proposes a control system for a tilt-rotor tricopter. This vehicle has 3 sets of propellers with one mounted on a servo to control the yaw movement. This results in asymmetry which requires a more complex control system to achieve stability. This paper proposes a gain scheduling PID control system designed for and implemented in such a tricopter. Flight stability was achieved by using decoupled control systems for positive and negative offsets of pitch and roll, and a separate controller for yaw. We present the step response of these controllers and show that the proposed system is able to stabilise the tricopter in flight
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