Abstract
We build a Kepler model of spacecraft gravity assist maneuver near a Venus-type planet and investigate its sensitivity to changes of the impact parameter. Analytical and numerical computations give similar results indicating a great increase of the trajectory final point shift under a small variation of the assigned spacecraft-planet distance.
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REFERENCES
R. Jehn, BepiColombo Mercury Cornerstone Consolidated Report on Mission Analysis. (MAS Working Paper No. 525, BC-ESC-RP-05500, ESOC, Robert-Bosch-Str. 5, 64293 Darmstadt, Germany, Issue 5.2 (26 January 2015) 0.
A. P. Yefremov, ‘‘General relativistic impact on the precision of BepiColombo gravity-assists,’’ Acta Astronautica 168, 44 (2020).
M. Ceriotti, Global Optimization of Multiple Gravity Assist Trajectories, PhD thesis (University of Glasgow, Dpt. Aerospace Engineering, 2010).
M. H. Kaplan, Modern Spacecraft Dynamics and Control (John Wiley and Sons, N.Y., 1976).
ACKNOWLEDGMENTS
The author thanks Dr. Alexandra A. Vorobyova for great assistance in numerical computations.
Funding
This study is done in the framework of the program to improve the competitiveness of the RUDN University among the world leading research and education centers in 2016–2020.
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Yefremov, A.P. Sensitivity of the Gravity Assist to Variations of the Impact Parameter. Gravit. Cosmol. 26, 118–123 (2020). https://doi.org/10.1134/S0202289320020127
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DOI: https://doi.org/10.1134/S0202289320020127