Event: AAS/AIAA Space Flight Mechanics Meeting 2003
Abstract:
Interpolation may be required for attitude data when repropagation
is either impossible or impractical. Nonlinearity of
kinematics and potential aliasing between revolutions are among
the unique challenges presented by the attitude motion.
Selections of the reference frame and attitude parameterization
become very important. It is possible to apply standard polynomial
interpolation techniques to the attitude data and, also, include the
angular velocity data in order to achieve a better accuracy and to
reduce potential for aliasing between revolutions. It is also
possible to employ interpolated polynomial trajectories for fixed
duration near optimal maneuver design and to achieve additional
optimization for spinners.
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Citation:
Tanygin, S., "Attitude Interpolation" AAS/AIAA Space Flight Mechanics Meeting, AAS 03-197, Ponce, Puerto Rico USA, 12 Feb 2003, accessible at https://comspoc.com/Resources/Content/Private/C-20220422T164452/Paper/Attitude-Interpolation.pdf.
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