TY - GEN
T1 - Model-based environment for verification and integration of micro-satellites
AU - Kuwahara, T.
AU - Tomioka, Y.
AU - Fukuda, K.
AU - Sugimura, N.
AU - Sakamoto, Y.
AU - Yoshida, K.
N1 - Funding Information:
This research was supported by Grant-in-Aid for Scientific Research on Innovative Areas KAKENHI:24760658 from the Ministry of Education, Culture, Sports, Science and Technology of Japan and by the Japan Society for the Promotion of Science (JSPS) through the "Funding Program for World-Leading Innovative R&D on Science and Technology (FIRST Program)," initiated by the Council for Science and Technology Policy (CSTP).
PY - 2013
Y1 - 2013
N2 - The Space Robotics Laboratory of Tohoku University has been developing multiples of microsatellites 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 micro-satellite project RISESAT, which is a 50kg class international scientific micro-satellite. 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.
AB - The Space Robotics Laboratory of Tohoku University has been developing multiples of microsatellites 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 micro-satellite project RISESAT, which is a 50kg class international scientific micro-satellite. 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.
KW - Assembly Integration and Test
KW - Micro-satellite
KW - Mission Control and Operation
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U2 - 10.3182/20130902-5-de-2040.00142
DO - 10.3182/20130902-5-de-2040.00142
M3 - Conference contribution
AN - SCOPUS:84899697418
SN - 9783902823465
T3 - IFAC Proceedings Volumes (IFAC-PapersOnline)
SP - 230
EP - 235
BT - 19th IFAC Symposium on Automatic Control in Aerospace, ACA 2013 - Proceedings
PB - IFAC Secretariat
T2 - 19th IFAC Symposium on Automatic Control in Aerospace, ACA 2013
Y2 - 2 September 2013 through 6 September 2013
ER -