Zuiani, Federico and Gibbings, Alison and Vetrisano, Massimo and Rizzi, Francesco and Martinez, Cesar and Vasile, Massimiliano (2012) Orbit determination and control for the European Student Moon Orbiter. Acta Astronautica, 79. pp. 67-78. ISSN 0094-5765
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This paper presents the preliminary navigation and orbit determination analyses for the European Student Moon Orbiter. The severe constraint on the total mission Delta nu and the all-day piggy-back launch requirement imposed by the limited available budget, led to the choice of using a low-energy transfer, more specifically a Weak Stability Boundary one, with a capture into an elliptic orbit around the Moon. A particular navigation strategy was devised to ensure capture and fulfil the requirement for the uncontrolled orbit stability at the Moon. This paper presents a simulation of the orbit determination process, based on an extended Kalman filter, and the navigation strategy applied to the baseline transfer of the 2011-2012 window. The navigation strategy optimally allocates multiple Trajectory Correction Manoeuvres to target a so-called capture corridor. The capture corridor is defined, at each point along the transfer, by back-propagating the set of perturbed states at the Moon that provides an acceptable lifetime of the lunar orbit. (C) 2012 Elsevier Ltd. All rights reserved.
|Keywords:||ESMO, weak stability boundary transfer, navigation, mission analysis, flight dynamics, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics|
|Subjects:||Technology > Mechanical engineering and machinery|
Technology > Motor vehicles. Aeronautics. Astronautics
|Department:||Faculty of Engineering > Mechanical and Aerospace Engineering|
Faculty of Science > Institute of Photonics
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|Depositing user:||Pure Administrator|
|Date Deposited:||03 Dec 2012 11:25|
|Last modified:||14 Jun 2013 19:16|
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