用于空中遥控实验的微型嵌入式旋翼机平台

J. Andersh, B. Mettler, N. Papanikolopoulos
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引用次数: 7

摘要

本文介绍了为便于微型旋翼机远程操作研究而开发的实验体系结构的硬件和软件系统。开发该平台的一个目标是将最小所需的传感器和电子设备放置在有效载荷有限的微型直升机上。机载硬件资源必须足以简化操作员的远程操作任务。在开发过程中,机载系统与明尼苏达大学交互式制导和控制实验室的基础设施相结合,以允许系统的方法来调查机载控制和制导增强。整个体系结构集成了允许各种估计、控制和制导算法方便地实现和测试的组件。在实验室环境中,Vicon跟踪系统用于精确确定直升机的姿态和方向,并在固定计算机上评估算法。这些准确的信息用于开发必要的度量标准,并在转换到实际情况之前评估不同算法的性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Miniature embedded rotorcraft platform for aerial teleoperation experiments
This paper describes the hardware and software systems that make up an experimental architecture developed to facilitate teleoperation research for miniature rotorcraft. One objective in developing this platform is to place the minimum required sensors and electronics onboard a miniature helicopter with limited payload. The onboard hardware resources must be sufficient to simplify the teleoperation task for the operator. While being developed, the onboard system is coupled with the infrastructure at the Interactive Guidance and Control Lab at the University of Minnesota to allow for a systematic approach to the investigation of onboard control and guidance augmentations. The overall architecture integrates components that allow a variety of estimation, control and guidance algorithms to be conveniently implemented and tested. In the lab environment, a Vicon tracking system is used to accurately determine a helicopter's pose and orientation and evaluate algorithms on stationary computers. This accurate information is used to develop the necessary metrics and evaluate the performance of different algorithms before transition to real-world situations.
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