Please use this identifier to cite or link to this item:
https://hdl.handle.net/2440/71926
Type: | Conference paper |
Title: | Small-satellite propulsion system modelling and simulation of orbital navigation determination; A feasibility study |
Author: | Zhang, L. Anvar, A. |
Citation: | Proceedings of the 19th International Congress on Modelling and Simulation (MODSIM2011), 12 to 16 December 2011, Perth, Western Australia / F. Chan, D. Marinova and R. S. Anderssen (eds.): pp.1119-1124 |
Publisher: | The Modelling and Simulation Society of Australia and NZ |
Publisher Place: | Australia |
Issue Date: | 2011 |
ISBN: | 9780987214317 |
Conference Name: | International Congress on Modelling and Simulation (19th : 2011 : Perth, Australia) |
Editor: | Chan, F. Marinova, D. Anderssen, R.S. |
Statement of Responsibility: | Lize Zhang and Amir Anvar |
Abstract: | The size and weight of Satellites are currently being miniaturised in order to meet the purpose of lowering cost and saving production time. For this situation, a type of Small-Satellite known as the CubeSat has been identified. This kind of small-satellite is 10 cm3 cube of less than 1.33kg. Due to its limitations on overall mass and dimensions, the CubeSat uses nanotechnology components for the interior design. Therefore, an appropriate design is a crucial aspect of any CubeSat project. According to space vehicle research and development criteria, the simulation and modelling of the subsystems of CubeSat is both significant and necessary. This paper investigates a feasibility study and demonstrates the simulation of Small-Satellite orbital navigation determination and Propulsion system modelling. |
Keywords: | Small-Satellite CubeSat Propulsion Modelling Orbital Simulation |
Rights: | Copyright © 2011 The Modelling and Simulation Society of Australia and New Zealand Inc. All rights reserved. |
Published version: | http://www.mssanz.org.au/modsim2011/C1/zhang.pdf |
Appears in Collections: | Aurora harvest 5 Mechanical Engineering conference papers |
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