How Do Conic Sections Relate to Orbital Mechanics?

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SUMMARY

The discussion centers on the mathematical relationship between conic sections and orbital mechanics, specifically how the eccentricity of conic sections correlates with the energy of orbits under inverse-square-law forces like gravity. The eccentricity is defined as \( e = \frac{\sin(\alpha)}{\sin(\beta)} \), where \( \alpha \) is the angle of the intersecting plane and \( \beta \) is the angle of the cone. According to Marion and Thornton's "Classical Dynamics of Particles and Systems," the eccentricity of an orbit is given by \( e = \sqrt{1 + \frac{2E \ell^{2}}{\mu k}} \), linking the angles of conic sections to orbital energy. This establishes a definitive mathematical connection between the geometry of conic sections and the dynamics of orbits.

PREREQUISITES
  • Understanding of conic sections (circle, ellipse, parabola, hyperbola)
  • Familiarity with orbital mechanics and gravitational forces
  • Knowledge of angular momentum and energy in physics
  • Basic grasp of mathematical relationships involving sine functions
NEXT STEPS
  • Study the concept of eccentricity in greater detail, particularly in relation to conic sections
  • Explore the implications of inverse-square-law forces in orbital mechanics
  • Research the mathematical derivations in "Classical Dynamics of Particles and Systems" by Marion and Thornton
  • Investigate potential generalizations of the relationship for other types of central forces
USEFUL FOR

Students and professionals in physics, particularly those focused on classical mechanics, orbital dynamics, and mathematical physics. This discussion is beneficial for anyone looking to deepen their understanding of the interplay between geometry and dynamics in celestial mechanics.

Ackbach
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If you think about a double-napped cone, and the various non-degenerate sections you can get with it:

1. Circle
2. Ellipse
3. Parabola
4. Hyperbola,

you can see that there is a progression here: increasing angle $\alpha$ that the intersecting plane makes with the horizontal. To be clear about this, $\alpha$ is not the angle that the normal to the intersecting plane makes with the horizontal, but the angle that the plane itself makes with the horizontal.

It's also true that for an inverse-square-law force, such as gravity (in the classical limit), this same progression describes increasing amounts of energy in the resulting orbit. I've long thought there must be some mathematical relationship between the two. And there is, through the eccentricity. The eccentricity of a conic section is defined as
$$e= \frac{ \sin( \alpha)}{ \sin( \beta)},$$
where $\alpha$ is the angle I've already defined, and $\beta$ is the angle that the cone makes with the horizontal.

According to Marion and Thornton's Classical Dynamics of Particles and Systems, 4th Ed., p. 304, Eq. (8.40), you also have that the eccentricity of an orbit under the gravitational force is equal to
$$e= \sqrt{1+ \frac{2E \ell^{2}}{ \mu k}},$$
where $E$ is the total energy, $\ell$ is the angular momentum, $\mu$ is the reduced mass
$$\mu= \frac{m_{1}m_{2}}{m_{1}+m_{2}},$$
and $k=Gm_{1}m_{2}$ (the numerator of the gravitational force law, although it could also be $q_{1}q_{2}/(4 \pi \epsilon_{0})$, I suppose, for a Coulomb force.)

Hence, we have that
$$ \frac{ \sin^{2}( \alpha)}{ \sin^{2}( \beta)}=1+ \frac{2E \ell^{2}}{ \mu k}.$$
So the relationship between the angle of the conic section and the energy of the orbit is that the square of the sine of the conic section angle is affinely related to the total energy.
 
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Greg Bernhardt said:
Thanks @Ackbach, what math forum can we move this to?
I would say Classical Physics.
 
I wonder if there is a similar relationship, more general, for any central force instead of specifically an inverse-square central force.
 

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