四旋翼无人机控制策略综述

IF 1.2 Q3 ENGINEERING, MECHANICAL FME Transactions Pub Date : 2023-01-01 DOI:10.5937/fme2303298s
Brajesh Singh, Awadhesh Kumar, G. Kumar
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引用次数: 0

摘要

四旋翼无人机(uav)近年来由于其在民用和军事领域的广泛应用而获得了极大的关注。它是一个高度非线性和欠驱动的系统,并且是户外飞行;由于阵风和其他环境因素,它总是受到外部干扰。该控制策略的实施具有计算时间长、不确定性大、逼近误差大、训练数据量大等缺点。在发展四旋翼机的主要挑战之一是设计一个有效和可靠的控制系统。本文综述了四旋翼飞行器的各种控制策略,并对其性能进行了评价。综述了传统的控制技术,如PID(比例-积分-导数)和LQR(线性二次调节器)和现代控制策略,如自适应和模糊控制。对各种控制策略进行了比较分析,提出了主要挑战和未来发展方向。本研究为研究人员和工程师设计四旋翼飞行器控制系统提供了有益的指导。
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Comprehensive review of various control strategies for quadrotor unmanned aerial vehicles
The Quadrotor Unmanned Aerial Vehicles (UAVs) have gained significant attention in recent years due to their versatile applications in civilian and military sectors. It is a highly nonlinear and underactuated system and an outdoor flight; it is always subjected to external disturbances due to wind gusts and other environmental factors. Implementing the control strategies could be improved in terms of high computational time, uncertainty, approximation error, and a large amount of training data. One of the major challenges in the development of quadrotors is the design of an efficient and reliable control system. This paper presents a comprehensive review of various control strategies for quadrotors and evaluates their performance. The review includes classical control techniques such as PID (Proportional-Integral-Derivative) and LQR (Linear Quadratic Regulator) and modern control strategies such as adaptive and fuzzy control. Comparative analysis of various control strategies has been presented with key challenges and future directions. This study provides a useful guide for researchers and engineers in the design of control systems for quadrotors.
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来源期刊
FME Transactions
FME Transactions ENGINEERING, MECHANICAL-
CiteScore
3.60
自引率
31.20%
发文量
24
审稿时长
12 weeks
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