Software Integration of an IMU Sensor to a CubeSat Platform Based on CSP (CubeSat Space Protocol)

Sergio-Fernando Barrera-Molano, Javier-Enrique Méndez-Gómez, Dib-Ziyari Salek-Chaves
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Abstract

The development and use of nanosatellites have increased in recent years. Space programs were exclusive to governments with significant capital. Now, nanosatellites have changed the orbital ecosystem and have allowed new regions and a wide range of industries to position themselves in the so-called new space, a growing sector that democratizes the commercialization of space thanks to a smaller, more agile, and affordable technology. Nanosatellites have similar capabilities to their conventional counterparts but are commonly used for highly specific missions such as Earth observation, telecommunications, and meteorology. The complex development of a nanosatellite requires solving different engineering problems to assembly and integrate all hardware and software components into a small space. It requires the monitoring, control, and operation of the satellite’s features from the ground segment. One major challenge is the development of satellite mission control software for both space and ground segments in limited-time scheduled missions. This article describes the integration process of an EPSON M-G364PDCA Inertial Measurement Unit (IMU) to a CubeSat platform nanosatellite based on the Danish company GomSpace devices and a CSP protocol. The result is a hardware implementation and software development by the Colombian Air Force (FAC) team as part of the FACSAT-2 program. The integration of these components into the space and ground segment contributes to solve one challenge in the development of control software for space missions, as described above, and becomes the first approach for Colombian space nanosatellites software development. In addition, this research presents the Colombian Air Force configuration for space mission subsystems on the CSP network, the software development for the main on-board computer based on a NanoMind A3200 to setup the IMU —controlled and monitored from the ground segment through a CSP terminal on a Linux server—, and setup telemetry data from space to be sent periodically to the ground segment and stored locally in a MongoDB database for its subsequent visualization and analysis.
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基于 CSP(立方体卫星空间协议)的 IMU 传感器与立方体卫星平台的软件集成
近年来,超小型卫星的开发和使用日益增多。太空计划是拥有大量资金的政府的专属项目。现在,超小型卫星已经改变了轨道生态系统,使新的地区和广泛的行业能够在所谓的新空间中占据一席之地,由于技术更小、更灵活、更经济实惠,这一不断增长的领域实现了空间商业化的民主化。超小型卫星具有与传统卫星类似的功能,但通常用于地球观测、电信和气象学等高度特定的任务。超小型卫星的开发十分复杂,需要解决不同的工程问题,将所有硬件和软件组件组装和集成到一个狭小的空间内。它要求从地面段对卫星的功能进行监测、控制和操作。其中一个主要挑战是在有限的时间计划任务中为空间和地面段开发卫星任务控制软件。本文介绍了将 EPSON M-G364PDCA 惯性测量单元(IMU)集成到基于丹麦 GomSpace 公司设备和 CSP 协议的 CubeSat 平台超小型卫星的过程。作为 FACSAT-2 计划的一部分,哥伦比亚空军(FAC)团队进行了硬件实施和软件开发。如上所述,将这些组件集成到空间和地面段有助于解决空间任务控制软件开发中的一个难题,并成为哥伦比亚空间超小型卫星软件开发的第一种方法。此外,本研究还介绍了哥伦比亚空军在 CSP 网络上对空间飞行任务子系统的配置,基于 NanoMind A3200 的主机载计算机的软件开发,以设置 IMU(通过 Linux 服务器上的 CSP 终端从地面段进行控制和监测),以及设置从空间定期发送到地面段的遥测数 据,并将其本地存储在 MongoDB 数据库中,以便随后进行可视化和分析。
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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