Design of decoupling and nonlinear PD controller for cruise control of a quadrotor

H. Arrosida, Rusdhianto Effendi, T. Agustinah, Josaphat Pramudijanto
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引用次数: 4

Abstract

Quadrotor is often used to accomplish various missions related to surveillance, territory mapping, search and rescue, and other purposes. Quadrotor is a nonlinear system with multiple input multiple output and has stability issue due to external disturbance. These characteristics lead to difficulty in cruise control of quadrotor automatically. Decoupling method is used to eliminate the interaction of other control on rotational motion, then the roll, pitch, and yaw angle can be controlled independently. Nonlinear PD controller is obtained from invers model of control signal on a quadrotor and it is used to control the translational motion in x and y axis with nonlinear dynamics because of the influence the rotational angle. Simulation results show that the proposed method can eliminate the control interaction of roll, pitch and yaw angle, hence it works like single input single output system and translational motion on x and y axis can achieve the expected trajectory precisely.
四旋翼飞行器巡航控制解耦与非线性PD控制器设计
四旋翼飞行器通常用于完成与监视、领土测绘、搜救和其他目的有关的各种任务。四旋翼飞行器是一种多输入多输出的非线性系统,由于外界干扰存在稳定性问题。这些特点导致四旋翼飞机自动巡航控制困难。采用解耦方法消除其他控制对旋转运动的影响,实现横摇、俯仰和偏航角的独立控制。非线性PD控制器是由四旋翼控制信号的逆模型得到的,用于控制四旋翼在x轴和y轴上的平移运动,该运动由于旋转角度的影响而具有非线性动力学。仿真结果表明,该方法消除了横摇、俯仰和偏航角的控制交互作用,使其像单输入单输出系统一样工作,并且在x轴和y轴上的平移运动可以精确地实现预期的轨迹。
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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