Design of unmanned semi-autonomous smart probe for near earth space research operations

Evren Daglarli, E. Aribas
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Abstract

To conduct studies related to our planet and its atmosphere at high altitudes above 100 km from the ground requires to overcome great challenges. These studies can include meteorological, geographical and astrophysical missions. In this paper, we designed a high altitude unmanned semi-autonomous probe with helium gas balloon for general purpose near Earth space studies. Also hardware architecture of our proposed system includes high performance computing module, Low-level control systems, propulsion/steering mechanisms, radio telemetry system, real-time measurement and data acquisition system, fail-safe mechanisms and real-time vision system. 3D solid design of the system contains helium gas balloon, main flight capsule (craft), peripheral equipment (e.g. cameras, battery packs, radio antenna, etc.) to be connected to the craft and payload capsule. In the future, our probe can be customized according to the other specified missions.
近地空间研究作业无人半自主智能探测器设计
在距离地面100公里以上的高空进行与地球及其大气有关的研究需要克服巨大的挑战。这些研究可以包括气象、地理和天体物理任务。本文设计了一种用于近地空间通用研究的高空无人半自主氦气球探测器。此外,我们提出的系统硬件架构包括高性能计算模块,低级控制系统,推进/转向机构,无线电遥测系统,实时测量和数据采集系统,故障安全机制和实时视觉系统。该系统的三维实体设计包含氦气气球、主飞行舱(飞行器)、连接到飞行器和有效载荷舱的外围设备(如相机、电池组、无线电天线等)。在未来,我们的探测器可以根据其他指定的任务进行定制。
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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