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
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;
Conference_Titel :
Recent Advances in Space Technologies (RAST), 2011 5th International Conference on
Conference_Location :
Istanbul
Print_ISBN :
978-1-4244-9617-4
DOI :
10.1109/RAST.2011.5966968
