Bypass maneuver by radial boosting impulse

1Avdeev, VV, 2Khorolskyi, PG
1Oles Honchar National University of Dnipropetrovsk, Dnipropetrovsk, Ukraine
2Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2002, 8 ;(4):043-048
Section: Spacecraft Dynamics and Control
Publication Language: Ukrainian
A linear model of the bypass of a cosmic object by an Earth's satellite is developed. This model gives a possibility to construct an effective algorithm for calculating the energy consumption in bypassing a dangerous area depending on the motion parameters of both objects. 
Keywords: bypassing a dangerous area, motion parameters, radial boosting impulse
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