Analytical Solutions for J3, J4, J5 and Third Body Perturbations for Orbit Propagation
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https://pure.strath.ac.uk/portal/en/datasets/analytical-solutions-for-j3-j4-j5-and-third-body-perturbations-for-orbit-propagation(354f9b2a-d1d5-4f51-9545-e963251f1e40).html
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资源简介：
Analytical solutions to the motion of the spacecraft subject to J3, J4, J5 and third body perturbations, expressed in non-singular equinoctial orbital elements. The solutions are reported in MATLAB files.
提供机构：
University of Strathclyde
创建时间：
2018-08-10
