Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/79574
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dc.contributor.authorLau, Ziruien
dc.contributor.authorLow, Kay Soonen
dc.contributor.authorGoh, Shu Tingen
dc.date.accessioned2014-10-28T07:48:46Zen
dc.date.accessioned2019-12-06T13:28:32Z-
dc.date.available2014-10-28T07:48:46Zen
dc.date.available2019-12-06T13:28:32Z-
dc.date.copyright2014en
dc.date.issued2014en
dc.identifier.citationGoh, S. T., Lau, Z. R., & Low, K. S. (2014). An optimization method for nano-satellite and pico-satellite separation through a two mass-one spring system. Advances in the astronautical sciences, 150, 723-732.en
dc.identifier.urihttps://hdl.handle.net/10356/79574-
dc.description.abstractThis paper studies the picosatellite ejection system from a nanosatellite, using one spring two mass ejection model. It is desired that both satellites maintain a long communication time after separation though they do not carry propulsion system. Moreover, the picosatellite is required to return to nanosatellite communication range in a given time period. The dynamic motion of the ejection system has been derived. The impact of ejection location, force and direction on the communication and separation time is studied. Results show that a continuous satellite communication could be maintained if the picosatellite is ejected in perpendicular to the flight path direction. However, the possible collision between the two satellites is to be taken into consideration.en
dc.format.extent13 p.en
dc.language.isoenen
dc.rights© 2014 American Astronautical Society. This paper was published in Advances in the Astronautical Sciences and is made available as an electronic reprint (preprint) with permission of American Astronautical Society. The paper can be found at the following official URL: [http://www.researchgate.net/publication/260821673_An_Optimization_Method_for_Nano-satellite_and_Pico-satellite_Separation_through_a_Two_Mass-One_Spring_System]. One print or electronic copy may be made for personal use only. Systematic or multiple reproduction, distribution to multiple locations via electronic or other means, duplication of any material in this paper for a fee or for commercial purposes, or modification of the content of the paper is prohibited and is subject to penalties under law.en
dc.subjectDRNTU::Engineering::Electrical and electronic engineering::Satellite telecommunicationen
dc.titleAn optimization method for nano-satellite and pico-satellite separation through a two mass-one spring systemen
dc.typeConference Paperen
dc.contributor.schoolSchool of Electrical and Electronic Engineeringen
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen
dc.contributor.conference2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013en
dc.description.versionPublished versionen
dc.identifier.urlhttp://www.researchgate.net/publication/260821673_An_Optimization_Method_for_Nano-satellite_and_Pico-satellite_Separation_through_a_Two_Mass-One_Spring_Systemen
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