Development of a high-speed software package for calculating the trajectory of launching a spacecraft into a geostationary orbit using the gravitational field of the moon with visualization of calculations

Heading: 
Spacecraft Dynamics and Control
1Serdiuk, OA, 1Izhko, VA, 1Arzhannikov, EV
1Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
Kosm. nauka tehnol. 2004, 10 ;(Supplement1):059-062
https://doi.org/10.15407/knit2004.01s.059
Publication Language: Russian
Abstract: 
The method of deducing small satellites into a geostationary orbit using the gravitational field of the Moon is considered. It is proposed to use software developed for project calculations of gravitational maneuver.
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