This work develops orbital dynamics using a Newtonian equation, revealing perihelion precession in a refined model.
This work develops the dynamical sector of the Simple Gravity framework using a Newtonian-type equation of motion in the nonlinear scalar field. The resulting orbital dynamics naturally produce perihelion precession, yielding a value equal to one-sixth of the relativistic prediction. This identifies the need for a refined dynamical description. This is the third paper in the Simple Gravity series.
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Ednilson Rodrigues (2026) studied this question.
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