implementation of a differential geometric filter for spacecraft formation orbit estimation

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ID: 236373
2012
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Abstract
The differential geometric filter is implemented to estimate the absolute and relative positions of the spacecraft in a formation. The extended Kalman Filter is also implemented as a benchmark for the differential geometric estimation. Only relative positions between the spacecraft are measured. Relative positions are measured using a wireless local positioning system (WLPS) installed in all spacecraft. Two different scenarios are studied: (1) the observations include WLPS measurements only and (2) the observations include WLPS measurements in addition to measurements for the absolute position of one spacecraft made by a radar that takes measurements from the earth’s surface. Results show that the differential geometric estimation has better stability performance and a faster convergence rate compared to the extended Kalman filter.
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goh2012internationalimplementation Use this key to autocite in the manuscript while using SciMatic Manuscript Manager or Thesis Manager
Authors ;Shu Ting Goh;Ossama Abdelkhalik;Seyed A. (Reza) Zekavat
Journal shanghai kou qiang yi xue = shanghai journal of stomatology
Year 2012
DOI
10.1155/2012/910496
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