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Control System Design of an Ultra-Small Deep Space Probe

机译：超小型深空探头的控制系统设计

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It's a grand opportunity to build new small deep space probe called Shinen2, developed by Kyushu Institute of Technology (KIT), in corporation with the different companies and institutions of engineering in Kagoshima University (Japan), NASA Johnson Space Center, was launched by the rocket H-IIA of Japan Aerospace Exploration Agency (JAXA) with Hayabusa 2, on December 3, 2014 in Tanegashima. This project involves Japanese students and foreigners, permitted a multi-cultural environment and an excellent tools for education. The students are in charge for the design, assembly, integration, tests of the space probe subsystems, and build-up of the existing ground stations facilities for tracking the telemetry data of Shinen2. It will enhance capacity building for the students, and scientific research for upcoming studies. The main approach to carry out the main mission of space probe. In parallel, to develop each subsystem of Shinen2: structure design, system bus architecture including the Communication Control Unit CCU, Power Control Unit PCU specifications, and new Particle Pixel Detector PPD for deep space radiation exploration. The development period for the space probe was only one year; it was extremely a short term. The mass budget and size were strictly limited while requiring a higher reliability. This paper describe a control system design for a small deep space probe which was developed to implement different missions and to satisfy the various requirements listed below.
机译：这是一个盛大的机会，建立新的小型空间探头，称为Shinen2，由九州理工学院（套件）开发，在鹿儿岛大学（日本）的不同公司和工程机构，NASA Johnson Space Center，由此推出日本航空航天探测机构（JAXA）火箭H-IIA与Hayabusa 2，2014年12月3日在塔尼卓。该项目涉及日本学生和外国人，允许多种文化环境和优秀的教育工具。学生负责设计，装配，集成，空间探测子系统的测试，以及现有地站的积聚，用于跟踪Shinen2的遥测数据。它将提高学生的能力建设，以及即将到来的研究的科学研究。开展空间探头主要任务的主要方法。并行开发Shinen2的每个子系统2：结构设计，系统总线架构，包括通信控制单元CCU，功率控制单元PCU规格，以及用于深空辐射探测的新型粒子像素检测器PPD。太空探针的发展期仅为一年;这是一个非常短的术语。大规模预算和规模严格限制，同时需要更高的可靠性。本文描述了一种用于小型深度空间探头的控制系统设计，该探头是开发的，实现了不同的任务，满足下面列出的各种要求。

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