Model-based simulation and verification environment for space plug-and-play avionics

Toshinori Kuwahara, Kazuya Yoshida, Yuji Sakamoto, Yoshihiro Tomioka, Kazufumi Fukuda, Nobuo Sugimura

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Recently small satellite development activities became popular throughout the world and the number of satellites being developed and launched a year is becoming larger. The Space Robotics Laboratory of Tohoku University has been developing multiples of micro-satellites for years and has gathered experiences in their development, verification, integration, and operation. SRL has recently started development of model-based simulation, verification and integration environment to realize rapid and cost-effective development of reliable micro-satellites. The conceptual design and its functionality have been verified through the real-life 50kg class micro-satellite projects. The developed environment can be utilized in different configurations depending on requirements in each satellite development phase. This environment is designed to be modular and very flexible and can be utilized for other micro-satellites and possibly even much smaller space system projects in the future. The forth micro-satellite of SRL, which is named RISESAT (Rapid International Scientific Experiment Satellite), introduces Space Plug-and- Play Avionics standard for payload instruments' electrical architecture. By applying a virtual system integration technology, remote integration of satellite components spread all over the world via internet becomes possible without getting together at a certain place. In this way the integration of a variety of scientific instruments becomes simple and the effort required can be dramatically reduced. According to this background, SRL started investigation of extending above mentioned model-based simulation environment for SPA compatible instruments. This environment shall enable software-based simulation and early functional verification of the SPA devices together with the satellite's bus system. This will improve the rapid and cost-effective development performance of small satellites which introduces SPA technology. Copyright

Original languageEnglish
Title of host publication64th International Astronautical Congress 2013, IAC 2013
PublisherInternational Astronautical Federation, IAF
Pages4282-4287
Number of pages6
ISBN (Print)9781629939094
Publication statusPublished - 2013 Jan 1
Event64th International Astronautical Congress 2013, IAC 2013 - Beijing, China
Duration: 2013 Sep 232013 Sep 27

Publication series

NameProceedings of the International Astronautical Congress, IAC
Volume6
ISSN (Print)0074-1795

Other

Other64th International Astronautical Congress 2013, IAC 2013
CountryChina
CityBeijing
Period13/9/2313/9/27

ASJC Scopus subject areas

  • Aerospace Engineering
  • Astronomy and Astrophysics
  • Space and Planetary Science

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