Classical Dynamics of Particles and Systems · Problem 8-20

Dynamics of a System of Particles — Marion & Thornton

Physics — Mechanics · central-force-time-average-elliptical-orbit

Problem

For a particle moving in an elliptical orbit with semimajor axis aa and eccentricity ε\varepsilon, show that ⟨(a/r)4cos⁡θ⟩=ε/(1−ε2)5/2\langle (a/r)^4 \cos\theta \rangle = \varepsilon/(1-\varepsilon^2)^{5/2} where the angular brackets denote a time average over one complete period.

Related theory

Browse the problem library