Physics
Scientific paper
Sep 1983
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1983cemec..31...43b&link_type=abstract
Celestial Mechanics (ISSN 0008-8714), vol. 31, Sept. 1983, p. 43-51.
Physics
8
Force Distribution, Gravitational Fields, Orbit Calculation, Orbital Mechanics, Three Dimensional Motion, Field Theory (Physics), Linear Equations, Partial Differential Equations
Scientific paper
Any two of the components X, Y, and Z of an autonomous force field which gives rise to the space orbits F(x, y, z) = c1, G(x, y, z) = c2 are related by a partial differential equation with coefficients depending on the functions F and G. This is a generalization of the corresponding equation for planar orbits (Bozis, 1983). The above partial differential equation is accompanied by the algebraic linear equation in X, Y, and Z expressing the fact that the force vector is lying in the osculating plane at each point of the orbit. The two equations constitute a generalization of the corresponding Szebehely's equations in the three dimensional space (Erdi, 1982). The generalization is meant in the sense that the dynamical system is not necessarily assumed to be conservative.
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