Исследование возможности непрямого перелета на ограниченную орбиту…
Инженерный журнал: наука и инновации
# 3
⋅
2016 9
Study the possibility of indirect flight into the restricted
orbit around the Earth—Moon’s L2 libration point
© M.S. Guskova
1
, S.A. Bober
1,2
, S.A. Aksenov
1,2
1
Moscow Institute of Electronics and Mathematics, National Research University
Higher School of Economics, Moscow, 124458, Russia
2
Space Research Institute RAS, Moscow, 117997, Russia
The paper analyzes the possibility of flight into the orbit around the translunar libration
point using gravity-assist maneuver near the Moon.
The orbits, which spacecraft can
enter without the use of intermediate maneuvers after the flyby of the Moon, are studied.
The flight from a parking low-Earth orbit into different orbits is simulated. Color maps of
characteristics dependent on the parameters of the flyby point and the map showing the
areas on the plane corresponding to the quasi-halo orbit, moving on which the spacecraft
does not go to the penumbra of the Moon are constructed.
Ключевые слова:
libration point, gravity-assist maneuver, lissajous orbit, quasi-halo
orbit.
REFERENCES
[1]
Folta D.C., Pavlak, T.A., Haapala A.F., Howel K.C., Woodard M.A.
Acta
Astronautica,
2014, no. 94 (1), рp. 421–433.
[2]
Burns J.O., Kring D.A., Hopkins J.B., Norris S., Lazio T.J. W., Kasper J.
Advances in Space Research
, 2013, no. 52 (2), рp. 306–320.
[3]
Farquhar R.W. The control and use of libration-point satellites.
Technical Report
R-346.
NASA, 1970.
[4]
Howell K.C., Pernicka H.J.
Journal of Guidance, Control, and Dynamics,
1993,
no. 16 (1), pp. 151–159.
[5]
Bober S.A., Aksenov S.A., Nikolaeva Yu.A. Issledovanie zavisimosti formy
ogranichennoy orbity kosmicheskogo apparata ot nachalnogo vektora
sostoyaniya v okrestnosti tochki libratsii L2 sistemy Solntse–Zemlya [Study of
the Dependence of the Restricted Spacecraft Orbit Form on the Initial State
Vector in the Vicinity of the Sun – Earth’s L2 Libration Point].
Materialy
Vosemnadtsatogo nauchno-tekhnicheskogo seminara
“
Novye informatsionnye
tekhnologii v avtomatizirovannykh systemakh”
[Proceedings of the eighteenth
scientific and technical workshop “New Information Technologies in Automated
Systems”]. Moscow, 2015.
[6]
Nikolaeva Yu.A., Aksenov S.A., Dunham D.W. Raschet okon zapuska
kosmicheskogo apparata dlya traektorii Zemlya-tochka L2 sistemy Zemlya-Luna
[Calculation of Spacecraft Launch Time Constraints for the Earth — L2 Point
Trajectory of the Earth – Moon System].
Trudy mezhdunarodnoy nauchno-
prakticheskoy konferentsii “Innovatsionnye Informatsionnye Tekhnologii”
[Proceedings of the International Scientific-Practical Conference “Innovative
Information Technologies”]. Prague, 2013, pp. 22–26.
[7]
Fedorenko Yu., Aksenov S.A., Dunham D.W. Evaluation time visibility of the
spacecraft when moving around L2 libration point of the Earth – Moon system.
Materials of the International Scientific-Practical Conference
“
Innovative
information technologies”.
Prague, 2013, р. 2.