Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/54526
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dc.contributor.authorGay, Dexter Kai Wei.
dc.date.accessioned2013-06-21T06:38:09Z
dc.date.available2013-06-21T06:38:09Z
dc.date.copyright2013en_US
dc.date.issued2013
dc.identifier.urihttp://hdl.handle.net/10356/54526
dc.description.abstractThis report aims to research and improve on the Nanosatellite to achieve better attitude determination and control on the functioning satellite. This will improve the overall capabilities and the efficiency of the satellite in Plasma Pulse Thruster. The aim was to improve the efficiency of the overall system by 200% Research was done on the control circuit to look for ways and methods to improve the control circuit. The first improvement was done on the components. It is required to meet the standard specifications of the circuit. Second improvement was done by implementing a step-up control circuit at the input of the system. Testing was done using wire wrapping. This helped to boost the efficiency by 50%. Last improvement was the implementation of a full wave multiplier block into the circuit. But the circuit proven to be too many components to be fabricated into the system. The results of the report was to improve the efficiency to 150% instead of the originally intended of 200%. Further research is required to get the intended voltage efficiency of 200%en_US
dc.format.extent47 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University
dc.subjectDRNTU::Engineeringen_US
dc.titleDevelopment of an advanced nano-satellite VELOX-I – a micro-thruster systemen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorLow Kay Soonen_US
dc.contributor.schoolSchool of Electrical and Electronic Engineeringen_US
dc.description.degreeBachelor of Engineeringen_US
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Appears in Collections:EEE Student Reports (FYP/IA/PA/PI)
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