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タイトルValidation of a Low-Thrust Mission Design Tool Using Operational Navigation Software
本文(外部サイト)http://hdl.handle.net/2060/20170001479
著者(英)Knittel, Jeremy M.; Ellison, Donald H.; Williams, Ken; Stanbridge, Dale; Englander, Jacob A.
発行日2017-02-05
言語eng
内容記述Design of flight trajectories for missions employing solar electric propulsion requires a suitably high-fidelity design tool. In this work, the Evolutionary Mission Trajectory Generator (EMTG) is presented as a medium-high fidelity design tool that is suitable for mission proposals. EMTG is validated against the high-heritage deep-space navigation tool MIRAGE, demonstrating both the accuracy of EMTG's model and an operational mission design and navigation procedure using both tools. The validation is performed using a benchmark mission to the Jupiter Trojans.
NASA分類Astrodynamics
レポートNOAAS 17-204
GSFC-E-DAA-TN38473-1
権利Copyright, Distribution as joint owner in the copyright


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