TY - GEN
T1 - ITU-pSAT II
T2 - 5th International Conference on Recent Advances in Space Technologies, RAST 2011
AU - Koyuncu, Emre
AU - Baskaya, Elgiz
AU - Cihan, Melahat
AU - Isiksal, Soner
AU - Fidanoglu, Melih
AU - Akay, Caner
AU - Cetin, Aykut
AU - Karadag, Burak
AU - Kaya, Yigit
AU - Karyot, Berat
AU - Haciyev, Cingiz
AU - Ozkol, Ibrahim
AU - Kaya, Metin Orhan
AU - Inalhan, Gokhan
PY - 2011
Y1 - 2011
N2 - ITU-pSAT II project aims to design and develop standardized bus architecture and an ADCS for pico and nano sized satellites. In order for nano-satellites to perform more capable missions, precise attitude control and more capable bus designs are needed. ITU-PSAT II is considered as follow-on to the ITU-PSAT I project, it includes multi-purpose bus and a 3-axis controlled platform, which can be used in future missions with different payload configurations. ITU-pSAT II bus and ADCS operation architecture also embeds a health monitoring system in order to cooperatively detect and successfully handle the highly possible failure modes (such as sensor, actuator failures and errors). In this paper, we review the architecture of ADCS, its subcomponents and strategy of combining ADCS operation modes.
AB - ITU-pSAT II project aims to design and develop standardized bus architecture and an ADCS for pico and nano sized satellites. In order for nano-satellites to perform more capable missions, precise attitude control and more capable bus designs are needed. ITU-PSAT II is considered as follow-on to the ITU-PSAT I project, it includes multi-purpose bus and a 3-axis controlled platform, which can be used in future missions with different payload configurations. ITU-pSAT II bus and ADCS operation architecture also embeds a health monitoring system in order to cooperatively detect and successfully handle the highly possible failure modes (such as sensor, actuator failures and errors). In this paper, we review the architecture of ADCS, its subcomponents and strategy of combining ADCS operation modes.
KW - Attitude Determination and Control
KW - Failure Tolerant Attitude Control
KW - Hardware in the Loop
KW - Software in the Loop
UR - http://www.scopus.com/inward/record.url?scp=80052104747&partnerID=8YFLogxK
U2 - 10.1109/RAST.2011.5966887
DO - 10.1109/RAST.2011.5966887
M3 - Conference contribution
AN - SCOPUS:80052104747
SN - 9781424496143
T3 - RAST 2011 - Proceedings of 5th International Conference on Recent Advances in Space Technologies
SP - 500
EP - 505
BT - RAST 2011 - Proceedings of 5th International Conference on Recent Advances in Space Technologies
Y2 - 9 June 2011 through 11 June 2011
ER -