Orbit Intersection Question (classical mechanics)

In summary, a comet is going in a parabolic orbit and the points where it intersects Earth's orbit are given by: cos(theta)=-1+(2*p)/a where p is the perihelion distance of the comet.
  • #1
^_^physicist
235
1

Homework Statement


A comet is going in a parabolic orbit lying in the plane of Earth's Orbit. Regarding Earth's orbit as circular of radius "a," show that the points where the comet intersects Earth's orbit are given by:

cos(theta)= -1 + (2*p)/a where p is the perihelion distance of the comet defined at (theta)=0


Homework Equations


Circular orbit: eccenticinty = 0
Parabolic orbit, Energy = 0, eccentincity = 1

Differential equation of an orbit:

d^2(u)/d(theta)^2 + u = -1/(m*l^2*u^2)*f(u^-1), where f is the function of the central force, u= 1/r, where r is the radius, and l is the angular momentum per mass.

Another representation of the differential equation of an orbit (using energy, and only for an inverse-squared central attractive force):

(du/d(theta))^2 + u^2 = 2E/ml^2 + 2ku/(ml^2); conditions are the same, except k= GM.

The Attempt at a Solution


Ok my thought was the solve the differential equations, once I have the solutions set the equations equal to one another and show that the points are predicted by the equation given; however, I don't have enough information given to solve the diff. eqs.

Any other ideas? I am quite stumped.
 
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  • #2
^_^physicist said:
Any other ideas? I am quite stumped.

Stop using physics. This is a simple geometry problem: Find the intersection of a parabola and a circle. The only physical result that is needed is that the center of the circle and the focus of the parabola are the same point.
 
  • #3
You don't have to solve the equations of motion. The geometry of the orbits is already given to you. So it's just a geometry problem. Just write down the polar coordinate representations of the two curves and intersect them. It's REALLY easy.
 
  • #4
Thanks for the tips; and yes you were right it was so easy to just think of it in geometric terms.
 

Related to Orbit Intersection Question (classical mechanics)

1. What is an orbit intersection question in classical mechanics?

An orbit intersection question in classical mechanics refers to the problem of determining the point at which two orbiting bodies cross paths. This is an important concept in understanding the motion of celestial bodies, such as planets and satellites.

2. How is the orbit intersection point calculated?

The orbit intersection point is calculated using mathematical equations, such as Kepler's laws of planetary motion. These equations take into account the masses, velocities, and distances of the orbiting bodies to determine the point at which their paths intersect.

3. What are some real-life applications of orbit intersection questions?

Orbit intersection questions have various real-life applications, such as predicting the paths of comets and asteroids, planning space missions, and understanding the dynamics of celestial bodies in our solar system.

4. Can an orbit intersection point change over time?

Yes, an orbit intersection point can change over time due to various factors such as the gravitational pull of other bodies, changes in velocity or distance, and perturbations in the orbiting bodies' paths.

5. How does the concept of orbit intersection relate to the three-body problem?

The three-body problem is a classic problem in celestial mechanics that deals with the motion of three bodies, such as planets, in a gravitational system. The concept of orbit intersection is closely related to the three-body problem, as it involves the interaction and intersection of two orbiting bodies.

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