Control and stability analysis of quadcopter

Asma Katiar, Rabbia Rashdi, Z. Ali, Urooj Baig
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引用次数: 10

Abstract

Today's World is getting more addicted of robot's applications and autonomous vehicles due to their improved performance and higher accuracy. A quad copter belongs to the same family due to flight stability, light weight, durability in flight, and accurate maneuverability. This research is based on design of dynamics controller of a quadcopter during hovering manuever using PID and SMC (sliding mode control) control techniques. The simulation results show improved response as compared to the previous studies under the same input conditions.
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四轴飞行器控制与稳定性分析
当今世界越来越沉迷于机器人应用和自动驾驶汽车,因为它们的性能和精度都有所提高。由于飞行稳定性、重量轻、飞行耐久性和精确的机动性,四轴直升机属于同一家族。本研究以四轴飞行器悬停机动的动态控制器设计为基础,采用PID和滑模控制技术。仿真结果表明,在相同的输入条件下,系统的响应比以往的研究有了很大的提高。
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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