2005
DOI: 10.1109/tasc.2005.849643
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An integrated micro HTS system for energy storage and attitude control for three-axis stabilized nanosatellites

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Cited by 7 publications
(2 citation statements)
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“…In our previous paper, we concentrated on a small-capacity energy storage system for micro-satellites and demonstrated that a small-sized flywheel levitates and rotates above the HTS [8][9][10]. In the first design of the flywheel, the motor and bearing magnets were located in the same plane.…”
Section: Previous Resultsmentioning
confidence: 99%
“…In our previous paper, we concentrated on a small-capacity energy storage system for micro-satellites and demonstrated that a small-sized flywheel levitates and rotates above the HTS [8][9][10]. In the first design of the flywheel, the motor and bearing magnets were located in the same plane.…”
Section: Previous Resultsmentioning
confidence: 99%
“…The spindown time was very short, within several tens of seconds, and this short spin-down time appeared to be mainly due to air drag. Figure 6 shows the rotational speed according to the input current to the circuit at 12 V. The input power also contains the power consumption of the driver circuit [14]. It was difficult to measure the force-displacement relationship of the HTS bearing in this system because the flywheel including the HTS bearing was small and the levitation force was feeble.…”
Section: Methodsmentioning
confidence: 99%