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- W2078596716 abstract "A method for determining the fill fraction of a liquid in a spacecraft is described. A small motion is introduced about the center of mass of the spacecraft undergoing steady spin and/or thrust, and the resulting oscillations are sensed. The frequency, amplitude and phase of the oscillations are identified from the measurement data and compared with counterpart values predicted for the possible liquid quantities by a non-empirical computed model of the spacecraft dynamics. This method is not subject to the errors or uncertainties of previous empirical methods based on ground testing. It also has the advantage that it can be applied to spacecraft already in orbit as it does not depend on a specific means of excitation or any specialized sensor mounted in or near the liquid container, or any prior ground calibration. A typical method of excitation, sensing and data acquisition and a computation approach are described along with presentation of actual flight data. Determination of fill fraction with an error of <0.5%, and within the estimated measurement and modeling uncertainties of this method has been demonstrated by independent means, including comparison of predictcd versus actual depletion." @default.
- W2078596716 created "2016-06-24" @default.
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- W2078596716 date "1993-08-09" @default.
- W2078596716 modified "2023-09-23" @default.
- W2078596716 title "Determination of spacecraft liquid fill fraction" @default.
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- W2078596716 doi "https://doi.org/10.2514/6.1993-3727" @default.
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