TY - GEN
T1 - Information-driven systems engineering study of a formation flying demonstration mission using six CubeSats
AU - Subramanian, Giri P.
AU - Foust, Rebecca
AU - Chen, Derek
AU - Chan, Stanley
AU - Taleb, Younes
AU - Rogers, Dayne
AU - Kokkat, Jobin
AU - Bandyopadhyay, Saptarshi
AU - Morganz, Daniel
AU - Chung, Soon Jo
AU - Hadaegh, Fred Y.
N1 - Publisher Copyright:
© 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2015
Y1 - 2015
N2 - Small satellites are suitable for formationying missions where a large number of space- craft serve as distributed sensors for applications like synthetic aperture radar, interfer- ometry, etc. A survey of existing or proposed small satellite missions concludes that there is a dearth of formation ying missions using four or more spacecraft that require forma- tion maintenance. This paper presents a systems engineering based design of a formation ying technology demonstration mission that requires precise formation maintenance and reconfigurations and highlights the challenges that need to be overcome for its successful implementation. The goal of this paper is to provide directions for future research and development in spacecraft formation ying technologies.
AB - Small satellites are suitable for formationying missions where a large number of space- craft serve as distributed sensors for applications like synthetic aperture radar, interfer- ometry, etc. A survey of existing or proposed small satellite missions concludes that there is a dearth of formation ying missions using four or more spacecraft that require forma- tion maintenance. This paper presents a systems engineering based design of a formation ying technology demonstration mission that requires precise formation maintenance and reconfigurations and highlights the challenges that need to be overcome for its successful implementation. The goal of this paper is to provide directions for future research and development in spacecraft formation ying technologies.
UR - http://www.scopus.com/inward/record.url?scp=84971383349&partnerID=8YFLogxK
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U2 - 10.2514/6.2015-2043
DO - 10.2514/6.2015-2043
M3 - Conference contribution
AN - SCOPUS:84971383349
SN - 9781624103438
T3 - 53rd AIAA Aerospace Sciences Meeting
BT - 53rd AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 53rd AIAA Aerospace Sciences Meeting, 2015
Y2 - 5 January 2015 through 9 January 2015
ER -