On stability of orbit of artificial moon moving around a small celestial body perturbed by an external body

ISSN： 0038-0946

Source： Solar System Research, Vol.45, Iss.7, 2011-12, pp. : 657-662

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Calculation of the intermediate perturbed orbit from three or more positions of a small body on the celestial sphere

By Shefer V.

Solar System Research, Vol. 47, Iss. 1, 2013-01 ,pp. : 38-49

MAIK Nauka/Interperiodica

Access to resources Recommend Favorite

Dynamical parameters of spacecraft motion near small celestial body

By Pol’ V.

Solar System Research, Vol. 45, Iss. 7, 2011-12 ,pp. : 614-621

MAIK Nauka/Interperiodica

Access to resources Recommend Favorite

Earth–Moon Weak Stability Boundaries in the restricted three and four body problem

By Romagnoli Daniele Circi Christian

Celestial Mechanics and Dynamical Astronomy, Vol. 103, Iss. 1, 2009-01 ,pp. : 79-103

Springer Publishing Company

Access to resources Recommend Favorite

Hamiltonian Stability of Spin–Orbit Resonances in Celestial Mechanics

By Celletti Alessandra Chierchia Luigi

Celestial Mechanics and Dynamical Astronomy, Vol. 76, Iss. 4, 2000-04 ,pp. : 229-240

Springer Publishing Company

Access to resources Recommend Favorite

On the stability of artificial equilibrium points in the circular restricted three-body problem

By Bombardelli Claudio Peláez Jesus

Celestial Mechanics and Dynamical Astronomy, Vol. 109, Iss. 1, 2011-01 ,pp. : 13-26

Springer Publishing Company

Access to resources Recommend Favorite