Kinematics of tight transition of asteroid near Earth and it withdrawal in elementary sense
UDC
629.78.001.5:523.44Abstract
Article discusses about the problem of withdrawal asteroid by change the parameter pass, forming a new orbit, safe for subsequent long period of time. It is shown that a minimum distance of withdrawal as a control parameter gravity manoeuvre in the linear approach is completely defined by two vectors: geocentric velocity vector of the asteroid, and the vector of the targeting point, a given change in the current coordinates of the asteroid's approach and serves to correct the orbit.
Keywords:
asteroids, asteroid threatReferences
- Chesley S.R. Potential impact detection for near-Earth asteroids, The case of 99942 Apophis (2004 MN4 // I Proceeding IAU Symposium 229th, 2005. Cambridge: Cambridge University press, 2006. P. 215-228.
- Соколов Л.Л., Борисова Т.П., Васильев А.А., Петров Н.А. Свойства траекторий соударения астероидов с Землей // Астрономический вестник. 2013. Т. 47. №4. С. 1-7.
- Давлетшин Г.З. Активно-гравитационные маневры КА. М.: Машиностроение, 1980. 254 с.
- Бронштейн И.Н., Семендяев К.А. Справочник по математике. М.: Наука, 1967. 608 с.
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Dates
Submitted
October 19, 2013
Accepted
November 15, 2013
Published
December 30, 2013
How to Cite
[1]
Pol, V.G., Simonov, A.V., Kinematics of tight transition of asteroid near Earth and it withdrawal in elementary sense. Ecological Bulletin of Research Centers of the Black Sea Economic Cooperation, 2013, № 4, pp. 112–117.
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Copyright (c) 2013 Поль В.Г., Симонов А.В.
This work is licensed under a Creative Commons Attribution 4.0 International License.
