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dc.contributor.authorAllahvirdizadeh, Amir
dc.contributor.supervisorAhmed El-Mowafyen_US
dc.contributor.supervisorPeter Teunissenen_US
dc.contributor.supervisorKan Wangen_US

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.

dc.publisherCurtin Universityen_US
dc.titlePrecise Orbit Determination of CubeSatsen_US
curtin.departmentSchool of Earth and Planetary Sciencesen_US
curtin.accessStatusOpen accessen_US
curtin.facultyScience and Engineeringen_US
curtin.contributor.orcidAllahvirdizadeh, Amir [0000-0002-3722-4417]en_US

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