Attitude Determination System For Nano Satellite Using Extended Kalman Filter On Arm7tdmi Platform
Extended kalman filter (ekf) has been successfully utilized in satellites missions. However, in comparison to other attitude determination methods developed, it is one of the most computationally burdening algorithm and with the new development of using nano satellites which have limited electric...
| Main Author: | |
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| Format: | Thesis |
| Language: | English |
| Published: |
2014
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| Subjects: | |
| Online Access: | http://eprints.usm.my/62911/ http://eprints.usm.my/62911/1/14-Pages%20from%2000001783664.pdf |
| _version_ | 1848885117572874240 |
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| author | Keui, Adam Ain Mohd Poin |
| author_facet | Keui, Adam Ain Mohd Poin |
| author_sort | Keui, Adam Ain Mohd Poin |
| building | USM Institutional Repository |
| collection | Online Access |
| description | Extended kalman filter (ekf) has been successfully utilized in satellites missions.
However, in comparison to other attitude determination methods developed, it is one of
the most computationally burdening algorithm and with the new development of using
nano satellites which have limited electrical power, mass, space and usually budget, it
is essential to design an attitude determination system (ads) which conforms to this
limitation. Therefore, in this thesis, as a computational improvement on the innosat
project, the rcm3400 microcontroller of the ads is replaced with the arm7tdmi
based microprocessor to test its capability. The arm7tdmi has been chosen since
it is one of the well-known microprocessor used in various electronic equipment because
it is low power and robust. The embest s3cev40 development board used,
houses the s3c44b0x microprocessor which is an arm7tdmi microprocessor. The
testing is done by connecting the development board to a personal computer which
has been installed with the arm interface software based on visual basic 6.0. |
| first_indexed | 2025-11-15T19:17:30Z |
| format | Thesis |
| id | usm-62911 |
| institution | Universiti Sains Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-15T19:17:30Z |
| publishDate | 2014 |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | usm-629112025-10-08T01:36:29Z http://eprints.usm.my/62911/ Attitude Determination System For Nano Satellite Using Extended Kalman Filter On Arm7tdmi Platform Keui, Adam Ain Mohd Poin TK1-9971 Electrical engineering. Electronics. Nuclear engineering Extended kalman filter (ekf) has been successfully utilized in satellites missions. However, in comparison to other attitude determination methods developed, it is one of the most computationally burdening algorithm and with the new development of using nano satellites which have limited electrical power, mass, space and usually budget, it is essential to design an attitude determination system (ads) which conforms to this limitation. Therefore, in this thesis, as a computational improvement on the innosat project, the rcm3400 microcontroller of the ads is replaced with the arm7tdmi based microprocessor to test its capability. The arm7tdmi has been chosen since it is one of the well-known microprocessor used in various electronic equipment because it is low power and robust. The embest s3cev40 development board used, houses the s3c44b0x microprocessor which is an arm7tdmi microprocessor. The testing is done by connecting the development board to a personal computer which has been installed with the arm interface software based on visual basic 6.0. 2014-09 Thesis NonPeerReviewed application/pdf en http://eprints.usm.my/62911/1/14-Pages%20from%2000001783664.pdf Keui, Adam Ain Mohd Poin (2014) Attitude Determination System For Nano Satellite Using Extended Kalman Filter On Arm7tdmi Platform. Masters thesis, Perpustakaan Hamzah Sendut. |
| spellingShingle | TK1-9971 Electrical engineering. Electronics. Nuclear engineering Keui, Adam Ain Mohd Poin Attitude Determination System For Nano Satellite Using Extended Kalman Filter On Arm7tdmi Platform |
| title | Attitude Determination System For Nano Satellite Using Extended Kalman Filter On Arm7tdmi Platform |
| title_full | Attitude Determination System For Nano Satellite Using Extended Kalman Filter On Arm7tdmi Platform |
| title_fullStr | Attitude Determination System For Nano Satellite Using Extended Kalman Filter On Arm7tdmi Platform |
| title_full_unstemmed | Attitude Determination System For Nano Satellite Using Extended Kalman Filter On Arm7tdmi Platform |
| title_short | Attitude Determination System For Nano Satellite Using Extended Kalman Filter On Arm7tdmi Platform |
| title_sort | attitude determination system for nano satellite using extended kalman filter on arm7tdmi platform |
| topic | TK1-9971 Electrical engineering. Electronics. Nuclear engineering |
| url | http://eprints.usm.my/62911/ http://eprints.usm.my/62911/1/14-Pages%20from%2000001783664.pdf |