参考文献

[1]Brower D. and Clemence G M. Methods of Celestial Mechanics. Academic Press, New York and London, 1961. 2nd impr.: Academic Press, Orlando, San Diego, New York, 1985. （刘林，丁华译.天体力学方法.北京：科学出版社，1986）

[2]Beutler G. Methods of Celestial Mechanics. Springer-Verlag Berlin, Heideberg, 2005.

[3]Vinti J P. Orbital and Celestial Methods. AIAA Education Series, American Institute of Aeronautics and Astronautics, Inc., Reston, Virginia, 1998.

[4]Boccaletti D. Pucacco G. Theory of Orbits, Vol. 1～2, Springer-Verlag, Berlin, Heideberg, 1999.

[5]Kozai Y. The motion of a close earth satellite. Astron. J., 1959, 64(9): 367-377.

[6]刘林．人造地球卫星轨道力学．北京：高等教育出版社，1992．

[7]刘林．航天器轨道理论．北京：国防工业出版社，2000．

[8]刘林，胡松杰，王歆．航天动力学引论．南京：南京大学出版社，2006．

[9]Szebehely V. Theory of Orbit—The Restricted Problem of Three Bodies. Academic Press, New York, London，1967.

[10]Brown E W. Solar Introductory Treatise on Lunar Theory. Cambridge University Press, 1896.

[11]Murray C D. Dermott S F. Solar System Dynamics. Cambridge University Press, 1999.

[12]Gómez G. et al. Dynamics and Mission Design Near Libration Points, Vol. 1～4, World Scientific, singapore, New Jersey, London, Hong Kong, 2001.

[13]侯锡云，刘林．共线平动点的动力学特征及其在深空探测中的应用．宇航学报，2008，29（3）：461-466.

[14]刘林，侯锡云．深空探测器轨道力学．北京：电子工业出版社，2012.

[15]Whipple A L. Szebehely V. The Restricted Problem of n＋ν Bodies. Celest. Mech. 1984, 32(2): 137-144.

[16]Whipple A L. Equilibrium Solutions of the Restricted Problem of 2＋2 Bodies. Celest. Mech. 1984, 33(3): 271-294.