Manoeuvre to bypass a dangerous zone by a satellite with thruster of low tractive force and radial direction
Heading:
| 1Avdeev, VV 1Oles Honchar National University of Dnipropetrovsk, Dnipropetrovsk, Ukraine |
| Kosm. nauka tehnol. 2007, 13 ;(3):027-030 |
| https://doi.org/10.15407/knit2007.03.027 |
| Publication Language: Ukrainian |
Abstract: For the single-turn evasive manoeuvre, we obtained the dependence of distance in a predictable time point between a satellite on a near-circle orbit and the centre of a dangerous zone on the value of radial acceleration created by the propulsion system.
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| Keywords: acceleration, manoeuvre to bypass, propulsion system |
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