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Jagadeeshwar, Hemanth (author)The Delfi-n3Xt was the second nanosatellite developed at the Delft University of Technology, and launched in 2013. Its successor Delfi-PQ is expected to be launched in first half of 2019. The Attitude of a satellite can be referred to as its orientation in space with respect to inertial reference frame. The Delfi-n3Xt was the first satellite...master thesis 2018
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Vos, M. (author)Attitude determination and control is the estimation of the current orientation of a satellite and controlling or changing it in order to reach a desired orientation. In the current gener- ation of nano satellites an Attitude Determination and Control Subsytem (ADCS) plays an important roll and sometimes even critical roll. An ADCS is necessary...master thesis 2013
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Van den Berg, A.F.C. (author)Fault-tolerant On-Board Computer (OBC) software for the Delfi-n3Xt nanosatellite is needed in order to minimize the risk of failures that may occur while the satellite is operating in space. Failures may be OBC specific, but failures that affect the state of the entire satellite and influence the health of the data bus may occur as well. Some...master thesis 2012
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De Jong, J.P. (author)The objective of this thesis is to perform systems engineering, detailed (re-)design and testing of the structural and mechanisms subsystems and facilitate the production of components.master thesis 2012
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Tindemans, A.M. (author)System design of the communication subsystem of the Delfi-n3Xt nanosatellite. Delfi-n3Xt is the successor of the Delfi-C3 nanosatellite.master thesis 2010
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Go, S.Y. (author)Design of the different elements in the Structural Subsystem of Delfi-n3Xt. This is done by implementation of the lessons learned and solutions to problems encountered with Delfi-C3. First different options for CubeSats are considered and traded. Afterwards the detailed design is treated. Also the arrangement of the different subsystems and...master thesis 2009