Analytical mechanics
Motion in a central field, the Kepler problem
Explore orbits in an inverse-square gravitational field as the eccentricity e varies. Verify the conic form and classify elliptic, parabolic, and hyperbolic orbits.
Equipment
- Orbit model around a central mass with eccentricity slider e (0–0.95)
- Hamilton–Jacobi action surface S(q,t) drawn beside the orbit
- Rotatable canvas and parameter readout line
- Pause button to freeze the motion
Procedure
Watch the orbit as eccentricity changes
Drag the e slider from 0 toward 0.95. At e = 0 the orbit is a circle; increasing e flattens the ellipse, with the central mass at one focus. Compare the orbit shape with .
Gauge the angular speed along the orbit
Press Pause at several positions and rotate the canvas for a better view. The body moves fast near periapsis and slow near apoapsis — the area law: , i.e. conserved angular momentum.
Compare with the action surface S(q,t)
Look at the surface S(q,t) beside the orbit: its slope in q gives momentum . Change e and predict how the surface deforms, then check on the figure; note this surface is one discretized illustrative solution, not the general action.