| Title: | Electric orbit raising mission simulator |
| Authors: | Matteo Aquilano, Author |
| Material Type: | ISU internship report |
| Publisher: | Illkirch-Graffenstaden (France) : International Space University, 2015 |
| Size: | 1 electronic resource (42 p.) / col. ill. |
| Bibliography note: | Internship Report submitted to the International Space University in partial fulfillment of the requirements of the M.Sc. Degree in Space Studies./ Includes bibliographical references |
| Languages: | English |
| Description: | This report addresses the evaluation of the losses associated with different constraints that cannot be modeled directly in a typical low-thrust trajectories optimizer. These constraints can be directly related to the real spacecraft behavior or arising from operational constraints derived from the implementation strategy chosen. In order to simulate a more complete mission scenario, a MatLab interface between the optimizer and an orbital propagator has been developed |
| ISU program : | Master of Space Studies |
| Permalink: | https://isulibrary.isunet.edu/index.php?lvl=notice_display&id=9617 |
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 Aquilano, Matteo_INT report (3.36MB) Adobe Acrobat PDF |
