Modeling and Simulation of Quadrotor UAV Using PID Controller

Mehmet Karahan, C. Kasnakoğlu
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引用次数: 11

Abstract

Recent developments in sensor technology, actuators and energy storage devices provides opportunities for development of micro flying robots. This paper provides information about modeling and control of a Quadrotor. Proportional Integral Derivative (PID) controller is designed for altitude and attitude control of Quadrotor. Various simulations were performed and it could be interpreted that the PID controller is capable of tracking the desired reference values. Finally, the last section is devoted for discussing the results of each simulation.
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基于PID控制器的四旋翼无人机建模与仿真
传感器技术、执行器和能量存储装置的最新发展为微型飞行机器人的发展提供了机会。本文提供了有关建模和控制四旋翼的信息。针对四旋翼飞行器的高度和姿态控制,设计了比例积分导数(PID)控制器。进行了各种仿真,可以解释为PID控制器能够跟踪所需的参考值。最后,最后一节专门讨论每个模拟的结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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