Robe’s restricted problem of 2+2 bodies when the bigger primary is a Roche ellipsoid and the smaller primary is an oblate body

Theory of Orbits.

V. Szebehely · NASA Technical Reports Server (NASA) · 1967 · 1.3K citations

Orbit Determination, Geometry, Periodic Orbits +3

Methods of Celestial Mechanics.

R. S. Burington, Dirk Brouwer, G. M. Clemence · American Mathematical Monthly · 1962 · 267 citations

Celestial Mechanics, Orbit Determination, Orbital Dynamics +1

<i>Methods of Celestial Mechanics</i>

Dirk Brouwer, G. M. Clemence, Nicholas Chako · Physics Today · 1962 · 160 citations

Engineering, Celestial Mechanic, Classical Mechanic +2

Stationary solutions and their characteristic exponents in the restricted three-body problem when the more massive primary is an oblate spheroid

Ram Krishan Sharma, P. V. Rao · Celestial Mechanics and Dynamical Astronomy · 1976 · 150 citations

Restricted Three-body Problem, Physics, Massive Primary +4

Collinear equilibria and their characteristic exponents in the restricted three-body problem when the primaries are oblate spheroids

Ram Krishan Sharma, P. V. Rao · Celestial Mechanics and Dynamical Astronomy · 1975 · 82 citations

Restricted Three-body Problem, Collinear Equilibria, Geometry +6