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sUAS Swarm Navigation using Inertial, Range Radios and Partial GNSS

机译:Suas群航行使用惯性,范围收音机和部分GNSS

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Small Unmanned Aerial Systems (sUAS) operations are increasing in demand and complexity. Using multiple cooperative sUAS (i.e. a swarm) can be beneficial and is sometimes necessary to perform certain tasks (e.g., precision agriculture, mapping, surveillance) either independent or collaboratively. However, controlling the flight of multiple sUAS autonomously and in real-time in a challenging environment in terms of obstacles and navigation requires highly accurate absolute and relative position and velocity information for all platforms in the swarm. This information is also necessary to effectively and efficiently resolve possible collision encounters between the sUAS. In our swarm, each platform is equipped with a Global Navigation Satellite System (GNSS) sensor, an inertial measurement unit (IMU), a baro-altimeter and a relative range sensor (range radio). When GNSS is available, its measurements are tightly integrated with IMU, baro-altimeter and range-radio measurements to obtain the platform's absolute and relative position. When GNSS is not available due to external factors (e.g., obstructions, interference), the position and velocity estimators switch to an integrated solution based on IMU, baro and relative range measurements. This solution enables the system to maintain an accurate relative position estimate, and reduce the drift in the swarm's absolute position estimate as is typical of an IMU-based system. Multiple multi-copter data collection platforms have been developed and equipped with GNSS, inertial sensors and range radios, which were developed at Ohio University. This paper outlines the underlying methodology, the platform hardware components (three multi-copters and one ground station) and analyzes and discusses the performance using both simulation and sUAS flight test data.
机译:小无人驾驶航空系统(SUAS)业务需求和复杂性越来越大。使用多个合作SUAS(即群体)可以是有益的,有时需要执行独立或协作的某些任务(例如,精密农业,映射,监控)。然而,在障碍和导航方面,在挑战环境中自主地和实时控制多个SUA的飞行,需要对群体中的所有平台的高度准确的绝对和相对位置和速度信息。此信息也必须有效,有效地解决SUA之间可能的碰撞。在我们的群体中,每个平台都配备了全球导航卫星系统(GNSS)传感器,惯性测量单元(IMU),一个标准仪和相对范围传感器(范围无线电)。当GNSS可用时,其测量与IMU,Baro-Altimeter和范围无线电测量紧密集成,以获得平台的绝对和相对位置。当GNSS不可由于外部因素(例如,障碍物,干扰),位置和速度估计器切换到基于IMU,气压和相对距离测量结果的集成解决方案。该解决方案使系统能够维持准确的相对位置估计,并降低群体的绝对位置估计中的漂移,因为是基于IMU的系统的典型。已经开发了多个多功能数据收集平台,并配备了在俄亥俄大学开发的GNSS,惯性传感器和范围收音机。本文概述的基本方法中,平台硬件组件(3多直升机装有和一个地面站)和分析和讨论了使用模拟和SUAS飞行试验数据的性能。

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