An Autonomous Landing Simulation System for UAV Tracking Mobile Carriers Based on Visual Servo

Qinlin Li, Mohammad Arif Bin Ilyas, N. Kamarudin
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Abstract

With the development of information technology, the fields of aerospace, electronic information, navigation and positioning are constantly developing in the direction of intelligence. The UAV, as an important part of modern military equipment, has been rapidly developed and widely used, but currently UAVs are flying according to the way the vehicle is designed to be structured. However, with the development of technology, the way in which vehicle structures used to be designed, manufactured and assembled has changed considerably and is also playing an increasingly important role in different fields. The main objective of this paper is to investigate the design of a simulation system for UAV tracking and autonomous landing based on visual servoing. This paper addresses the shortcomings of the current UAV autonomous landing simulation technology and proposes a visual servo-based UAV tracking mobile carrier autonomous landing simulation system, which carries out motion simulation calculations such as motion trajectory measurement at the landing point and autonomous landing through the mobile carrier carried by the UAV autonomously. The simulation system does not affect the aircraft landing process, but also provides a new idea and method for the study of the autonomous landing mechanism of mobile carriers. The simulation system mainly consists of three basic structures: the UAV body, the mobile carrier and the visual servo; the simulation system mainly completes the autonomous landing process of the UAV carrier through two control methods: one is real-time motion control; the other is the tracking path parameter optimisation algorithm; the target attitude information is obtained for the landing simulation calculation under the two control methods. The system will provide a new way of thinking and a new method for the research of the UAV autonomous landing mechanism.
基于视觉伺服的无人机跟踪移动载体自主着陆仿真系统
随着信息技术的发展,航空航天、电子信息、导航定位等领域不断向智能化方向发展。无人机作为现代军事装备的重要组成部分,得到了迅速的发展和广泛的应用,但目前无人机的飞行方式是按照飞行器的设计结构进行的。然而,随着技术的发展,过去车辆结构的设计、制造和组装方式发生了很大的变化,并在不同的领域发挥着越来越重要的作用。本文的主要目的是研究基于视觉伺服的无人机跟踪与自主着陆仿真系统的设计。针对当前无人机自主着舰仿真技术的不足,提出了一种基于视觉伺服的无人机跟踪移动载体自主着舰仿真系统,该系统可自主进行着陆点运动轨迹测量等运动仿真计算,并通过无人机所携带的移动载体自主着陆。该仿真系统在不影响飞机着陆过程的前提下,为移动载体自主着陆机理的研究提供了一种新的思路和方法。仿真系统主要由无人机本体、移动载体和视觉伺服三个基本结构组成;仿真系统主要通过两种控制方式完成无人机载体的自主着陆过程:一种是实时运动控制;二是跟踪路径参数优化算法;获取目标姿态信息,用于两种控制方式下的着陆仿真计算。该系统将为无人机自主着陆机构的研究提供新的思路和方法。
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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