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The secular analytical solution of the orbital plane using Lindstedt-Poincaré method

  • Published:2017-11 Issue:10 Volume:60 Page:2166-2180
  • ISSN:0273-1177
  • Container-title:Advances in Space Research
  • language:en
  • Short-container-title:Advances in Space Research

Author:

Yu Shengxian,Zhao Changyin,Zhang Wei

Funder

National Defense Science and Technology Innovation Program of The Chinese Academy of Sciences

National Natural Science Foundation of China

Natural Science Foundation of Jiangsu Province

Publisher

Elsevier BV

Subject

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

Reference17 articles.

1. The long period motion of the plane of a distant circular orbit;Allan;Proc. Roy. Soc. Lond., Ser. A: Math. Phys. Sci.,1964

2. Long-term third-body effects via double averaging;Broucke;J. Guid. Contr. Dyn.,2003

3. ELP 2000-85: a semi-analytical lunar ephemeris adequate for historical times;Chapront-Touzé;Astron. Astrophys.,1988

4. Third-body perturbation in the case of elliptic orbits for the disturbing body;Domingos;Math. Problems Eng.,2008

5. A study of single- and double-averaged second-order models to evaluate third-body perturbation considering elliptic orbits for the perturbing body;Domingos;Math. Problems Eng.,2013

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