Can time on elliptical orbit be expressed analytically?

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In summary, elliptical orbits cannot be expressed analytically, but can be calculated with Kepler's equation.
  • #1
snorkack
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Can time on elliptical orbit be expressed analytically? Which relations are capable of analytic expression?
The distance from focus can be expressed as a function of position angle θ:
r=a(1-e2)/(1+e cos θ)
The length linearly along the ellipse famously cannot be expressed analytically.
The total time spent on ellipse depends on a alone (Kepler 3rd).
If the angular speed at any r of θ were known then the angular speed at any other r would be because r∂θ/∂t=cost for any a and e.
But is there any analytic expression to find r∂θ/∂t given a and e?
Also, is there any way to find
0θ∫∂θ/∂t, or 0t∫∂t/∂θ? These are different questions because many analytic expressions cannot be reversed.
 
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  • #2
Have you investigated Kepler’s second law of constant area speed for your problem already ?
 
  • #3
If your inverse square central force problem is governed by [tex]
\ddot r - r\dot \theta^2 = -\frac{K}{r^2}[/tex] with [itex]L = r^2\dot\theta[/itex] constant and [itex]\theta(0) = 0[/itex] then we have [tex]
L^2 = K\ell[/tex] where the semi-latus rectum [itex]\ell[/itex] of the elliptical orbit is given in terms of the semi-major axis [itex]a[/itex] and eccentricity [itex]0 \leq e < 1[/itex] by [tex]
\ell = a(1 - e^2).[/tex] We then have [tex]\begin{split}
Lt &= \int_0^t L\,dt \\
&= \int_0^{\theta(t)} r^2 \,d\theta \\
&= \int_0^\theta \frac{\ell^2}{(1 + e\cos \theta)^2}\,d\theta.\end{split}[/tex]
 
  • #4
Found the answer to two questions (out of the three).
Kepler equation:
M=E-e*sin E
where M is mean anomaly and E is an intermediate expression called "elliptic anomaly".
E can be expressed through true anomaly and vice versa:
sin E=√(1-e2)*sin θ/(1+e*cos θ)
tan θ/2=√((1+e)/(1-e))*tan E/2
Given E, or θ, finding M is straightforward.
Finding E (and thus θ) given M is an insoluble problem after over four centuries.
 
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  • #5
snorkack said:
Found the answer to two questions (out of the three).
Given E, or θ, finding M is straightforward.
Finding E (and thus θ) given M is an insoluble problem after over four centuries.
The answer to third question is also easy on some reflection.
While θ as a function of M is insoluble, M as a function of θ is soluble. But since M can be expressed as a function of θ, you can express ∂M/∂θ as function of θ - you can take a derivative of every function but you cannot take an integral of every function. But since ∂θ/∂M is a simple reciprocal of ∂M/∂θ, you can calculate it, as long as you are calculating it as a function of θ rather than M (which is insoluble).
 
  • #6
So do you have a result?
 

1. What is an elliptical orbit?

An elliptical orbit is a type of orbit in which an object, such as a planet or satellite, follows a path that is shaped like an ellipse. This means that the distance between the object and the body it is orbiting around varies throughout its orbit.

2. How is time on an elliptical orbit calculated?

Time on an elliptical orbit can be calculated using Kepler's laws of planetary motion. These laws state that the square of the orbital period of a planet is proportional to the cube of the semi-major axis of its orbit.

3. Can time on an elliptical orbit be expressed mathematically?

Yes, time on an elliptical orbit can be expressed analytically using Kepler's laws and other mathematical equations, such as the orbital velocity formula.

4. What factors affect the time on an elliptical orbit?

The time on an elliptical orbit is affected by the mass of the object being orbited, the eccentricity of the orbit, and the semi-major axis of the orbit. Other factors such as external forces and gravitational influences can also affect the time on an elliptical orbit.

5. Why is it important to understand the time on an elliptical orbit analytically?

Understanding the time on an elliptical orbit analytically is important for predicting the position and movement of objects in space. It also allows us to accurately calculate and plan for space missions, satellite orbits, and other astronomical events.

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