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Multidisciplinary design and flight testing of a remote gas/particle airborne sensor system

机译:远程气体/颗粒机载传感器系统的多学科设计和飞行测试

摘要

The main objective of this paper is to describe the development of a remote sensing airborne air sampling system for Unmanned Aerial Systems (UAS) and provide the capability for the detection of particle and gas concentrations in real time over remote locations. The design of the air sampling methodology started by defining system architecture, and then by selecting and integrating each subsystem. A multifunctional air sampling instrument, with capability for simultaneous measurement of particle and gas concentrations was modified and integrated with ARCAA’s Flamingo UAS platform and communications protocols. As result of the integration process, a system capable of both real time geo-location monitoring and indexed-link sampling was obtained. Wind tunnel tests were conducted in order to evaluate the performance of the air sampling instrument in controlled nonstationary conditions at the typical operational velocities of the UAS platform. Once the remote fully operative air sampling system was obtained, the problem of mission design was analyzed through the simulation of different scenarios. Furthermore, flight tests of the complete air sampling system were then conducted to check the dynamic characteristics of the UAS with the air sampling system and to prove its capability to perform an air sampling mission following a specific flight path.
机译:本文的主要目的是描述用于无人机系统(UAS)的遥感机载空气采样系统的开发,并提供在远程位置实时检测颗粒和气体浓度的功能。空气采样方法的设计始于定义系统架构,然后选择和集成每个子系统。多功能空气采样仪经过改进,可以同时测量颗粒和气体浓度,并与ARCAA的Flamingo UAS平台和通信协议集成在一起。作为集成过程的结果,获得了一个能够同时进行实时地理位置监视和索引链接采样的系统。进行风洞测试是为了在UAS平台的典型运行速度下,在受控的非平稳条件下评估空气采样仪器的性能。一旦获得了远程全功能空气采样系统,就可以通过模拟不同的情景来分析任务设计的问题。此外,随后对整个空气采样系统进行了飞行测试,以检查带有空气采样系统的UAS的动态特性,并证明其按照特定飞行路径执行空气采样任务的能力。

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