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- W2090717210 abstract "A graphical method that allows the selection of the attitude orientation of a spinner spacecraft prior to the application of a single fixed magnitude velocity change to effect a desired orbit transfer is presented. The selection of the final pointing vector along or opposite to which the desired Delta-V is applied, takes into account pointing errors due to initial attitude determination uncertainty and execution errors introduced during the rhumb line precession of the spin axis. The characterization of the target space in terms of any achieved orbit parameters of interest as well as the final pointing uncertainty is sufficient to determine the right final attitude that insures satisfaction of mission requirements." @default.
- W2090717210 created "2016-06-24" @default.
- W2090717210 creator A5049898921 @default.
- W2090717210 date "1984-08-17" @default.
- W2090717210 modified "2023-10-03" @default.
- W2090717210 title "A strawman targeting technique for spinner spacecraft in the presence of pointing uncertainty" @default.
- W2090717210 cites W2092894282 @default.
- W2090717210 doi "https://doi.org/10.2514/6.1984-1983" @default.
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