Abstract
A micro-piggyback satellite, "μ-LabSat", was launched by an H-IIA rocket on 14 December 2002. μ-LabSat is a bias momentum micro-satellite with two wheels, a configuration that is not normally capable of three-axis attitude maneuvers. This paper describes an algorithm that has been developed to enable such maneuvers and presents the results of its evaluation by numerical simulation and in-orbit experiment. © 2005 The Japan Society for Aeronautical and Space Sciences.
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Terui, F., Kimura, S., Nagai, Y., Yamamoto, H., Yoshihara, K., Yamamoto, T., & Nakasuka, S. (2005). Moon tracking attitude control experiment of a bias momentum micro satellite “μ-LabSat.” Transactions of the Japan Society for Aeronautical and Space Sciences, 48(159), 28–33. https://doi.org/10.2322/tjsass.48.28
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