Analysis of the change of orbital elements in the process of gravity assist-Reference-Cited by-同舟云学术

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Analysis of the change of orbital elements in the process of gravity assist

Published:2019-09 Issue:6 Volume:64 Page:1298-1316
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Liu Jingxi,Xu Bo,Zhang Lei

Funder

Basic Scientific Research Fund of National Defense

National Basic Research Program 973 of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference22 articles.

1. Battin, R.H., 1987. An introduction to the mathematics and methods of astrodynamics.

2. Buffington, B., 2014. Trajectory Design Concept for the Proposed Europa Clipper Mission (Invited). https://doi.org/10.2514/6.2014-4105. URL https://arc.aiaa.org/doi/abs/10.2514/6.2014-4105.

3. Tisserand-leveraging transfers;Campagnola;J. Guid. Control Dyn.,2014

4. A fast tour design method using non-tangent v-infinity leveraging transfer;Campagnola;Celestial Mech. Dyn. Astron.,2010

5. Chamberlin, A.B., 2019. Horizons web-interface. URL https://ssd.jpl.nasa.gov/horizons.cgi.

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1. Implementation of Euler-Lambert equation for determination of interplanetary trajectory to the planet Jupiter;XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration;2021

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