Precise Orbit Determination of CubeSats
| dc.contributor.author | Allahvirdizadeh, Amir | |
| dc.contributor.supervisor | Ahmed El-Mowafy | en_US |
| dc.contributor.supervisor | Peter Teunissen | en_US |
| dc.contributor.supervisor | Kan Wang | en_US |
| dc.date.accessioned | 2023-01-03T02:53:09Z | |
| dc.date.available | 2023-01-03T02:53:09Z | |
| dc.date.issued | 2022 | en_US |
| dc.identifier.uri | http://hdl.handle.net/20.500.11937/89922 | |
| dc.description.abstract |
CubeSats are faced with some limitations, mainly due to the limited onboard power and the quality of the onboard sensors. These limitations significantly reduce CubeSats' applicability in space missions requiring high orbital accuracy. This thesis first investigates the limitations in the precise orbit determination of CubeSats and next develops algorithms and remedies to reach high orbital and clock accuracies. The outputs would help in increasing CubeSats' applicability in future space missions. | en_US |
| dc.publisher | Curtin University | en_US |
| dc.title | Precise Orbit Determination of CubeSats | en_US |
| dc.type | Thesis | en_US |
| dcterms.educationLevel | PhD | en_US |
| curtin.department | School of Earth and Planetary Sciences | en_US |
| curtin.accessStatus | Open access | en_US |
| curtin.faculty | Science and Engineering | en_US |
| curtin.contributor.orcid | Allahvirdizadeh, Amir [0000-0002-3722-4417] | en_US |