Spacecraft relative attitude determination
A method to determine the relative attitudes between three spacecraft is developed. The method requires four direction measurements between the three spacecraft. The simulation results and covariance analysis show that the method's error falls within a three sigma boundary without exhibiting an...
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2013
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sg-ntu-dr.10356-995622020-03-07T13:24:49Z Spacecraft relative attitude determination Goh, Shu Ting Passerello, Chris E Abdelkhalik, Ossama School of Electrical and Electronic Engineering IEEE Aerospace Conference (2010 : Montana, US) DRNTU::Engineering::Electrical and electronic engineering A method to determine the relative attitudes between three spacecraft is developed. The method requires four direction measurements between the three spacecraft. The simulation results and covariance analysis show that the method's error falls within a three sigma boundary without exhibiting any singularity issues. A study of the accuracy of the proposed method with respect to the shape of the spacecraft formation is also presented. Accepted version 2013-08-06T04:20:11Z 2019-12-06T20:08:53Z 2013-08-06T04:20:11Z 2019-12-06T20:08:53Z 2010 2010 Conference Paper Goh, S. T., Passerello, C. E., & Abdelkhalik, O. (2010). 2010 IEEE Aerospace Conference. Spacecraft Relative Attitude Determination, 1-6. https://hdl.handle.net/10356/99562 http://hdl.handle.net/10220/13047 10.1109/AERO.2010.5446994 167984 en © 2010 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. The published version is available at DOI: [http://dx.doi.org/10.1109/AERO.2010.5446994]. application/pdf |
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DRNTU::Engineering::Electrical and electronic engineering Goh, Shu Ting Passerello, Chris E Abdelkhalik, Ossama Spacecraft relative attitude determination |
| description |
A method to determine the relative attitudes between three spacecraft is developed. The method requires four direction measurements between the three spacecraft. The simulation results and covariance analysis show that the method's error falls within a three sigma boundary without exhibiting any singularity issues. A study of the accuracy of the proposed method with respect to the shape of the spacecraft formation is also presented. |
| author2 |
School of Electrical and Electronic Engineering |
| author_facet |
School of Electrical and Electronic Engineering Goh, Shu Ting Passerello, Chris E Abdelkhalik, Ossama |
| format |
Conference or Workshop Item |
| author |
Goh, Shu Ting Passerello, Chris E Abdelkhalik, Ossama |
| author_sort |
Goh, Shu Ting |
| title |
Spacecraft relative attitude determination |
| title_short |
Spacecraft relative attitude determination |
| title_full |
Spacecraft relative attitude determination |
| title_fullStr |
Spacecraft relative attitude determination |
| title_full_unstemmed |
Spacecraft relative attitude determination |
| title_sort |
spacecraft relative attitude determination |
| publishDate |
2013 |
| url |
https://hdl.handle.net/10356/99562 http://hdl.handle.net/10220/13047 |
| _version_ |
1681048640264601600 |