Spacecraft spin axis attitude determination
A mathematical formulation of the spacecraft spin axis attitude determination problem in the form of a norm constrained-least-squares minimization problem is provided. The formulation has a mathematically transparent interpretation as a search for the optimal unit vector on the surface of the unit s...
محفوظ في:
| المؤلف الرئيسي: | |
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| مؤلفون آخرون: | |
| التنسيق: | article |
| منشور في: |
1992
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| الموضوعات: | |
| الوصول للمادة أونلاين: | https://eprints.kfupm.edu.sa/id/eprint/14025/1/14025_1.pdf https://eprints.kfupm.edu.sa/id/eprint/14025/2/14025_2.doc |
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| _version_ | 1864513383774027776 |
|---|---|
| author | Emara-Shabaik, H.E. |
| author2 | unknown |
| author2_role | author |
| author_facet | Emara-Shabaik, H.E. unknown |
| author_role | author |
| dc.creator.none.fl_str_mv | Emara-Shabaik, H.E. unknown |
| dc.date.none.fl_str_mv | 1992-04 2020 |
| dc.format.none.fl_str_mv | application/pdf application/msword |
| dc.identifier.none.fl_str_mv | https://eprints.kfupm.edu.sa/id/eprint/14025/1/14025_1.pdf https://eprints.kfupm.edu.sa/id/eprint/14025/2/14025_2.doc (1992) Spacecraft spin axis attitude determination. Aerospace and Electronic Systems, IEEE Transactions on, 28. |
| dc.language.none.fl_str_mv | en en |
| dc.publisher.none.fl_str_mv | IEEE |
| dc.relation.none.fl_str_mv | https://eprints.kfupm.edu.sa/id/eprint/14025/ |
| dc.rights.*.fl_str_mv | info:eu-repo/semantics/openAccess |
| dc.subject.none.fl_str_mv | Computer |
| dc.title.none.fl_str_mv | Spacecraft spin axis attitude determination |
| dc.type.none.fl_str_mv | Article PeerReviewed info:eu-repo/semantics/publishedVersion info:eu-repo/semantics/article |
| description | A mathematical formulation of the spacecraft spin axis attitude determination problem in the form of a norm constrained-least-squares minimization problem is provided. The formulation has a mathematically transparent interpretation as a search for the optimal unit vector on the surface of the unit sphere. Two algorithms are developed and compared by simulation. The results show a tradeoff between estimation accuracy and computational requirements. One algorithm is about three times more accurate than the other and is therefore recommended even though it requires about 20% more in computer storage and operations, and about 50% more in central processing unit time |
| eu_rights_str_mv | openAccess |
| format | article |
| id | KFUPM_08fea7b3836af49943b7e88649645f69 |
| identifier_str_mv | (1992) Spacecraft spin axis attitude determination. Aerospace and Electronic Systems, IEEE Transactions on, 28. |
| language_invalid_str_mv | en |
| network_acronym_str | KFUPM |
| network_name_str | King Fahd University of Petroleum and Minerals |
| oai_identifier_str | oai::14025 |
| publishDate | 1992 |
| publisher.none.fl_str_mv | IEEE |
| repository.mail.fl_str_mv | |
| repository.name.fl_str_mv | |
| repository_id_str | |
| spelling | Spacecraft spin axis attitude determinationEmara-Shabaik, H.E.unknownComputerA mathematical formulation of the spacecraft spin axis attitude determination problem in the form of a norm constrained-least-squares minimization problem is provided. The formulation has a mathematically transparent interpretation as a search for the optimal unit vector on the surface of the unit sphere. Two algorithms are developed and compared by simulation. The results show a tradeoff between estimation accuracy and computational requirements. One algorithm is about three times more accurate than the other and is therefore recommended even though it requires about 20% more in computer storage and operations, and about 50% more in central processing unit timeIEEE1992-042020ArticlePeerReviewedinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfapplication/mswordhttps://eprints.kfupm.edu.sa/id/eprint/14025/1/14025_1.pdfhttps://eprints.kfupm.edu.sa/id/eprint/14025/2/14025_2.doc (1992) Spacecraft spin axis attitude determination. Aerospace and Electronic Systems, IEEE Transactions on, 28. enenhttps://eprints.kfupm.edu.sa/id/eprint/14025/info:eu-repo/semantics/openAccessoai::140252019-11-01T14:03:48Z |
| spellingShingle | Spacecraft spin axis attitude determination Emara-Shabaik, H.E. Computer |
| status_str | publishedVersion |
| title | Spacecraft spin axis attitude determination |
| title_full | Spacecraft spin axis attitude determination |
| title_fullStr | Spacecraft spin axis attitude determination |
| title_full_unstemmed | Spacecraft spin axis attitude determination |
| title_short | Spacecraft spin axis attitude determination |
| title_sort | Spacecraft spin axis attitude determination |
| topic | Computer |
| url | https://eprints.kfupm.edu.sa/id/eprint/14025/1/14025_1.pdf https://eprints.kfupm.edu.sa/id/eprint/14025/2/14025_2.doc |