2007
DOI: 10.2514/1.25134
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Sizing/Optimization of a Small Satellite Energy Storage and Attitude Control System

Abstract: Public reporting burden Tor this collection ot ntormation is estimated to average 1 hour per response, including the time tor reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the colection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington Headquarters Services, Directorate for Information Operations and R… Show more

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Cited by 36 publications
(18 citation statements)
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“…The first two approaches use the available capacity equation presented in [14] while the third approach applies the usable capacity concept defined here. The designs were determined in the following order: first, an optimization with fixed rotor length was done, then, an optimization was done by changing the available capacity equation to the method from [14], and finally, a separate optimization was done for the old design.…”
Section: Numerical Example and Resultsmentioning
confidence: 99%
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“…The first two approaches use the available capacity equation presented in [14] while the third approach applies the usable capacity concept defined here. The designs were determined in the following order: first, an optimization with fixed rotor length was done, then, an optimization was done by changing the available capacity equation to the method from [14], and finally, a separate optimization was done for the old design.…”
Section: Numerical Example and Resultsmentioning
confidence: 99%
“…The first two approaches use the available capacity equation presented in [14] while the third approach applies the usable capacity concept defined here. The designs were determined in the following order: first, an optimization with fixed rotor length was done, then, an optimization was done by changing the available capacity equation to the method from [14], and finally, a separate optimization was done for the old design. This approach yielded three distinctly different point designs that are illustrated in Figure 5.15(f) and summarized in Table 5 The culmination of this effort yields the mass savings versus rotor length for different design alternatives as reflected in Figure 5.16.…”
Section: Numerical Example and Resultsmentioning
confidence: 99%
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