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Rutherford's extended formula and optimization of the gravity assists beam modeling in the Solar system
Author(s) -
Yu. F. Golubev,
А. В. Грушевский,
V. V. Koryanov,
А. Г. Тучин,
Д. А. Тучин
Publication year - 2021
Publication title -
preprint/preprinty ipm im. m.v. keldyša
Language(s) - English
Resource type - Journals
eISSN - 2071-2901
pISSN - 2071-2898
DOI - 10.20948/prepr-2021-6
Subject(s) - spacecraft , physics , aerospace engineering , interplanetary spaceflight , solar system , gravitation , planet , beam (structure) , classical mechanics , mechanics , plasma , astrobiology , astronomy , optics , engineering , solar wind , quantum mechanics
The extended Rutherford formula for the gravitational scattering is obtained. Semi-analytical guaranteeing estimates are presented for a sufficient number of a spacecraft’ virtual trajectories in a beam when simulating gravity assist maneuvers around the Solar system massive bodies which are forming the unceasing procedure for searching for the interplanetary ballistic scenarios. A special importance here is assured by the guaranteed synthesis of the bang-bang gravity assist maneuvers chains if it is necessary to change the asymptotic velocity of the spacecraft relative to the planet.

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