1990
DOI: 10.1086/191477
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On the problem of the HIPPARCOS reference frame

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Cited by 3 publications
(2 citation statements)
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“…Rigid rotations (spins) of SIM's reference frame are parts of the null space of a global astrometric solution (Lattanzi, Bucciarelli & Bernacca 1990;Makarov & Milman 2005), and, therefore, can not be determined from observations with SIM. They are confined to three low-order magnetic vector harmonics, while the vector field of proper motions caused by the secular acceleration is represented by the three electric harmonics of zero and first order.…”
Section: Discussionmentioning
confidence: 99%
“…Rigid rotations (spins) of SIM's reference frame are parts of the null space of a global astrometric solution (Lattanzi, Bucciarelli & Bernacca 1990;Makarov & Milman 2005), and, therefore, can not be determined from observations with SIM. They are confined to three low-order magnetic vector harmonics, while the vector field of proper motions caused by the secular acceleration is represented by the three electric harmonics of zero and first order.…”
Section: Discussionmentioning
confidence: 99%
“…The full covariance matrix could not be computed in Hipparcos, since the adopted solution was not global, but rather a three-step iterative procedure including the adjustment of one-dimensional abscissae coordinates and attitude (great circle reductions), adjustment of reference great circle zero points, and finally, a fit to astrometric parameters over the entire set of the great circle abscissae (sphere solution). The main reason for using this scheme was the practical difficulty of a least-squares solution on a global design matrix of over unknowns 5 6 # 10 ( Lattanzi et al 1990). …”
Section: Introductionmentioning
confidence: 99%