四轴飞行器控制与稳定性分析

2018 International Conference on Computing, Mathematics and Engineering Technologies (iCoMET) Pub Date : 2018-03-01 DOI:10.1109/ICOMET.2018.8346419

Asma Katiar, Rabbia Rashdi, Z. Ali, Urooj Baig

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引用次数: 10

摘要

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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Control and stability analysis of quadcopter

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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来源期刊

2018 International Conference on Computing, Mathematics and Engineering Technologies (iCoMET)

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