Main Property of the Jacobi Integral for Gravity Assist Maneuvers in the Solar System

In the context of the circular restricted three-body problem (RTBP), the search for the spacecraft’s asymptotic velocity for gravity assist maneuvers (GMs) can be performed using the Jacobi integral and the main property of the Jacobi integral constant for GMs, It is shown in the paper that the stan...

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Bibliographic Details
Published inSolar system research Vol. 53; no. 6; pp. 473 - 480
Main Authors Golubev, Yu. F., Grushevskii, A. V., Kiseleva, I. P., Koryanov, V. V., Tuchin, A. G., Tuchin, D. A.
Format Journal Article
LanguageEnglish
Published Moscow Pleiades Publishing 01.11.2019
Subjects
Astronomy
Astrophysics and Astroparticles
Astrophysics and Cosmology
Observations and Techniques
Physics
Physics and Astronomy
Planetology
Tisserand parameter
asymptotic velocity
gravity assist maneuver
Jacobi integral
restricted three-body problem
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Summary:In the context of the circular restricted three-body problem (RTBP), the search for the spacecraft’s asymptotic velocity for gravity assist maneuvers (GMs) can be performed using the Jacobi integral and the main property of the Jacobi integral constant for GMs, It is shown in the paper that the standard cumbersome way of traditional derivation of this property that is used in modern astrodynamics can be significantly simplified.
ISSN:0038-0946
1608-3423
DOI:10.1134/S0038094619060029