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|
1. Avdeev V. V., Khorolsky P. G. The energy expenditure of a spacecraft on a two-pulse maneuver to bypass a dangerous object. Tehnicheskaja mehanika, No. 1, 129—136 (2001) [in Russian].
2. Jakson M. P. Space surveillance satellite catalog maintenance. AIAA Pap., No. 1339, P. 9 (1990).
3. Jonson N. L., Nauer D. J. Orbital debris detection: Techniques and issues. AIAA Pap., No. 1330, 8 p. (1990).