DocumentCode
2492150
Title
The selenocentric orbit´s formation as one of guidance problems of spacecraft with low trust which accomplishes transport tasks in the Earth-Moon system
Author
Stariniva, O.L. ; Materova, I.L.
Author_Institution
Dept. of Flight vehicles, Samara State Aerosp. Univ., Korolev, Russia
fYear
2011
fDate
9-11 June 2011
Firstpage
875
Lastpage
878
Abstract
In paper it is investigated control laws choice and suited transfer low thrust lunar-center trajectories in the Earth-Moon system in limited three-body problem. Interactive steering methodology is found. For variable initial conditions mission duration and fuel mass are obtained. It is suggested approach of initial approximation choices to solve boundary tasks. It is given results of numerical modeling.
Keywords
aerospace control; numerical analysis; space research; Earth-Moon system; fuel mass; lunar-center trajectories; numerical modeling; selenocentric orbit formation; spacecraft guidance problems; variable initial conditions mission duration; Earth; Fuels; Gravity; Moon; Orbits; Space vehicles; Trajectory; control laws; modeling; numerical methods; spacecraft;
fLanguage
English
Publisher
ieee
Conference_Titel
Recent Advances in Space Technologies (RAST), 2011 5th International Conference on
Conference_Location
Istanbul
Print_ISBN
978-1-4244-9617-4
Type
conf
DOI
10.1109/RAST.2011.5966968
Filename
5966968
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