基于控制PID的小型无人机导航算法设计

Wenqi Wu
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引用次数: 0

摘要

无人机导航系统应用的目的是准确判断无人机在水平空间中的位置,保证其能够按照预期的设定航线飞行。虽然过去提出的惯性卫星(GPS)导航系统设计符合传统市场的发展需求,但在新时代,随着小型无人机进入研究人员的视野,专家们开始对导航控制系统的对策和算法进行新的设计。因此,本文在了解现有小型无人机导航算法的设计方案和基本原理的同时,分析了如何结合专家PID导航控制律的设计方法,设计并实现基于专家PID的小型无人机导航算法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design of Small Unmanned Aerial Vehicle Navigation Algorithm Based on Control PID
The purpose of the application of UAV navigation system is to accurately judge the position of UAV in horizontal space and ensure that it can fly according to the expected set course. Although the inertia-satellite (GPS) navigation system design proposed in the past is in line with the development needs of the traditional market, in the new era, as small unmanned aerial vehicles enter the field of vision of researchers, experts begin to carry out a new design of the countermeasures and algorithms of the navigation control system. Therefore, this paper analyzes how to design and implement the navigation algorithm of small unmanned aerial vehicles (U AVs) based on expert PID combined with the design method of expert PID navigation control law while understanding the design scheme and basic principles of the existing navigation algorithm of small unmanned aerial vehicles (UAVs).
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