1918
DOI: 10.1086/122696
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Cited by 15 publications
(18 citation statements)
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“…As noted already by Aitken (1918), when an orbit is incomplete, several theoretical orbits will provide satisfactory fits. Two possible responses to this circumstance are: 1) scan parameter space to find the global minimum (e.g., Hartkopf et al 1989) and assume that this orbit is the closest achievable approximation to the truth; or 2) scan parameter space to make a complete census of acceptable orbits and then compute an appropriate average of the individual mass determinations (e.g., Schaefer et al 2006).…”
Section: Bayesian Estimationmentioning
confidence: 73%
“…As noted already by Aitken (1918), when an orbit is incomplete, several theoretical orbits will provide satisfactory fits. Two possible responses to this circumstance are: 1) scan parameter space to find the global minimum (e.g., Hartkopf et al 1989) and assume that this orbit is the closest achievable approximation to the truth; or 2) scan parameter space to make a complete census of acceptable orbits and then compute an appropriate average of the individual mass determinations (e.g., Schaefer et al 2006).…”
Section: Bayesian Estimationmentioning
confidence: 73%
“…(1) is easy to calculate, statistical tests indicate that the resulting ellipse seems inferior to that calculated from SDP. Despite what Aitken (1964), and others, have stated, it seems worthwhile to pay the computational price for a method such as SDP, where the minimization criterion bears a strict relationship to the fitted ellipse and convergence, unlike what may occur with nonlinear least squares, is guaranteed.…”
Section: Discussionmentioning
confidence: 96%
“…Interpolating curves were drawn for the P.A. (t) and the separation (t) (Aitken 1964). These curves were constructed to vary smoothly with time and to yield a consistent value for the constant of areas, 2 ave ½DðP:A:Þ=Dt, across equally spaced time intervals.…”
Section: Computation Of Orbital Elementsmentioning
confidence: 99%