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- W2313929478 abstract "Thermal ly induced deformations of flexible appendages have long been one of the largest disturbance source s for earth orbiting satellites . A number of attempts have been made to characterize these disturbances but to date there is no universal model that can accu rately extend to new solar wing designs. This paper introduces a novel approach for identify ing the size of the snap disturbance based on in -flight telemetry data and statistically quantifies them into models for new space missions. This novel identification algorithm uses in flight telemetry data and processes it through an inverse model of spacecraft dynamics to derive the snap disturbance torque. This paper describes the identification algorithm, numerical result s a nd modeling process to predict new in -flight thermal snap transient s. In particular, this method was used to extend the snap torque model from a previously -launched satellite with 5 -panel solar wings to a new one with 6 panel wings. The prediction matched up excellently with on -orbit data. ." @default.
- W2313929478 created "2016-06-24" @default.
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- W2313929478 date "2003-06-22" @default.
- W2313929478 modified "2023-09-26" @default.
- W2313929478 title "Thermal Snap Disturbance Identification via In-Flight Data" @default.
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- W2313929478 doi "https://doi.org/10.2514/6.2003-5825" @default.
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