基于STM32单片机的航天器姿态传感器软硬件建模技术

Aleksandr Kulakov, Aleksandr V. Smirnov
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引用次数: 0

摘要

目前,复杂技术对象(CTO)的硬件和软件建模概念得到了快速发展,包括在航天工业中。这类对象的主要特征是存在复杂的、有时是异构结构的实时控制系统。在考虑CTO建模时,“X-In-the-Loop”的概念在国外文学中非常流行。在用于航天器建模(SC)的专门软件(SW)中,值得强调的是具有足够的文档来理解其工作的开源软件和Internet上活跃的社区。本文提出了一种基于Project 42 (SC建模软件)和单片机STM32的软硬件建模技术。为了在该技术的框架内与MC STM32一起工作,使用了集成开发环境IAR嵌入式工作台。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Technology of Hardware and Software Modeling of Spacecraft Attitude Sensors Based on STM32 Microcontrollers
Currently, the concept of hardware and software modeling of complex technical objects (CTO) has received rapid development, including in the space industry. The main feature of such objects is the presence of real-time control systems with a complex and sometimes heterogeneous structure. The concept of “X-In-the-Loop” has gained great popularity in foreign literature when considering modeling of CTO. Among the specialized software (SW) for modeling spacecraft (SC), it is worth highlighting open source SW that has sufficient documentation to understand their work and an active community on the Internet. This report proposes a hardware-software modeling technology based on Project 42 (SW for modeling of SC) and microcontroller (MC) STM32. To work with MC STM32 within the framework of this technology, the integrated development environment IAR Embedded Workbench is used.
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