NASA NTRS · 19730035780
Nonlinear estimation theory applied to the interplanetary orbit determination problem.
Abstract
The performance of a second order filter which is identical to the algorithm developed by Athans et al. (1968) for the scalar case is evaluated through numerical simulation of a Jupiter flyby mission. The observations used in the simulation are on-board measurements of the angle between Jupiter and a fixed star taken at discrete time intervals. In the numerical study, the influence of each of the second order terms is evaluated.
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Tapley, B. D., Choe, C. Y.. 1972-01-01. Nonlinear estimation theory applied to the interplanetary orbit determination problem.. https://ntrs.nasa.gov/citations/19730035780
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