Skip to article frontmatterSkip to article content

8Two Body Problem: Kepler revisited

Newton must have realized that his analysis of the Kepler laws was not 100% correct. After all, the sun is not fixed in space and even though its mass is much larger than any of the planets revolving it, it will have to move under the influence of the gravitational force by the planets. Take for example, the sun and earth as our system. By the account of Newton’s third law, the Earth exerts also a force on the Sun. Therefore, the Sun has to move as well; thus, we must revisit the Earth-Sun analysis and incorporate that the Sun isn’t fixed in space.

Two-particle system, with an action/reaction pair of forces.

Figure 1:Two-particle system, with an action/reaction pair of forces.

The two-body problem is stated hereby as:

Particle m1m_1 feels an external force F1\vec{F}_1 and an interaction force from particle two, F21\vec{F}_{21}. Similarly for particle m2m_2: it feels an external force F2\vec{F}_2 and an interaction force from particle one, F12\vec{F}_{12}.

Consider the situation in the figure:

m1x¨1=F1+F21m_1 \ddot{\vec{x}}_1 = \vec{F}_1 + \vec{F}_{21}
m2x¨2=F2+F12m_2 \ddot{\vec{x}}_2 = \vec{F}_2 + \vec{F}_{12}

Add the two equations and use N3: F12=F21\vec{F}_{12} = - \vec{F}_{21}:

m1x¨1+m2x¨2=F1+F2m_1 \ddot{\vec{x}}_1 + m_2 \ddot{\vec{x}}_2 = \vec{F}_1 + \vec{F}_{2} \Leftrightarrow
P˙=F1+F2\dot{\vec{P}} = \vec{F}_{1} + \vec{F}_2

with Pp1+p2\vec{P} \equiv \vec{p}_1 + \vec{p}_2. In words, it is as if a particle with (total) momentum P\vec{P} responds to the external forces but does not react to internal forces (the mutual interaction).

8.1Center of Mass

It is now logical to assign the total mass M=m1+m2M=m_1+m_2 to this fictitious particle. It has momentum p1+p2\vec{p}_1+\vec{p}_2 which we can also couple to its mass MM and assign a velocity V\vec{V} to it such that P=MV\vec{P}=M\vec{V}. Furthermore, if this fictitious mass has velocity V\vec{V}, we can also assign a position to it. After all, V=dRdt\vec{V} = \frac{d\vec{R}}{dt}, which gives us the recipe for the position R\vec{R}.

Its velocity V\vec{V} and position R\vec{R} then follow as:

V=m1v1+m2v2m1+m2=m1dx1dt+m2dx2dtm1+m2R=m1x1+m2x2m1+m2+C\begin{split} \vec{V} &= \frac{m_1 \vec{v}_1 + m_2 \vec{v}_2 }{m_1 + m_2} \\ &= \frac{m_1 \frac{d\vec{x}_1}{dt} + m_2 \frac{d\vec{x}_2}{dt} }{m_1 + m_2}\\ \\ \Rightarrow \vec{R} &= \frac{m_1 \vec{x}_1 + m_2 \vec{x}_2}{m_1 + m_2} +\vec{C} \end{split}

In the last equation, we have an integration constant in the form of a vector, C\vec{C}. We are free to choose it as we want: its precise value does not affect the velocity V\vec{V} nor the momentum P\vec{P} of our fictitious particle.

It makes sense, to choose: C=0\vec{C} = 0 and thus define as position of the particle:

R=m1x1+m2x2m1+m2\vec{R} = \frac{m_1 \vec{x}_1 + m_2 \vec{x}_2}{m_1 + m_2}

Why?

We have a few arguments:

  1. if the particles are actually each half of a real particle, we obviously require that R\vec{R} is the position of the real particle.
  2. If the particles are separate by a small distance, we would like to have the fictitious particle somewhere in between the two. Moreover, if the two particles are identical, it makes sense to have the fictitious particle right in between them: the system is symmetric.

Where, in general is the position R\vec{R}? That can be easily seen from the figure below.

Center of Mass and relative coordinates.

Figure 2:Center of Mass and relative coordinates.

We rewrite the definition of R\vec{R}:

Rm1x1+m2x2m1+m2=x1+m2m1+m2(x2x1)\vec{R} \equiv \frac{m_1 \vec{x}_1 + m_2 \vec{x}_2}{m_1 + m_2} = \vec{x}_1 + \frac{m_2}{m_1 + m_2} \left ( \vec{x}_2 - \vec{x}_1\right )

Thus, the last part of the above equation tells us: first go to m1m_1 and then, ‘walk’ a fraction m2m1+m2\frac{m_2}{m_1 + m_2} of the line connecting m1m_1 and m2m_2. If you have done that, you are at position R\vec{R}.
Note: if m1=m2m_1 = m_2 this recipe indeed brings us right between the two particles.
Further note: the position of MM is always on the line from m1m_1 to m2m_2. If m1m_1 is much larger than m2m_2, it will be located close to m1m_1 and vice versa.

We call this position the center of mass, or CM for short. Reason: if we look at the response of our two particle system to the forces, it is as if there is a particle MM at position R\vec{R} that has all the momentum of the system.

It turns out to be convenient to define relative coordinates with respect to the center of mass position (see also the figure above):

r1x1R and r2x2R\vec{r}_1 \equiv \vec{x}_1 - \vec{R} \text{ and } \vec{r}_2 \equiv \vec{x}_2 - \vec{R}

Via the external forces, we can ‘follow’ the motion of the center of mass position, i.e. R\vec{R}. From the CM as new origin, we can find the position of the two particles.

A helpful rule is found from:

m1r1+m2r2==m1(x1R)+m2(x2R)=m1x1+m2x2(m1+m2)R=0\begin{array}{l} m_1 \vec{r}_1 + m_2 \vec{r}_2 = \\ =m_1 \left ( \vec{x}_1 - \vec{R} \right ) + m_2 \left ( \vec{x}_2 - \vec{R} \right ) \\ =m_1 \vec{x}_1 + m_2 \vec{x}_2 - (m_1 + m_2 ) \vec{R} = 0 \end{array}
m1r1+m2r2=0\Rightarrow m_1 \vec{r}_1 + m_2 \vec{r}_2 = 0

This has an important consequence: if we know r1\vec{r}_1, we know r2\vec{r}_2, and vice versa. Note: the directions of r1\vec{r}_1 and r2\vec{r}_2 are always opposed and the center of mass R\vec{R} is located somewhere on the connecting line between m1m_1 and m2m_2.

Note 2: in the case of no external forces F1=F2=0\vec{F}_1=\vec{F}_2=0 and only internal forces F120\vec{F}_{12} \neq 0 the CM moves according to N1 with constant velocity (P˙=0)(\dot{\vec{P}}=0).

8.2Energy

In terms of relative coordinates, we can write the kinetic energy as a part associated with the CM and a part that describes the kinetic energy with respect to the CM, i.e., ‘an internal kinetic energy.’

Ekin12m1v12+12m2v22=12m1(r˙1+R˙)2+12m2(r˙2+R˙)2=12MR˙2+12m1r˙12+12m2r˙22\begin{array}{rcl} E_{kin} &\equiv &\frac{1}{2} m_1 v_1^2 + \frac{1}{2} m_2 v_2^2 \\ &= &\frac{1}{2} m_1 \left ( \dot{\vec{r}}_1 + \dot{\vec{R}} \right )^2 + \frac{1}{2} m_2 \left ( \dot{\vec{r}}_2 + \dot{\vec{R}} \right )^2 \\ &= &\frac{1}{2} M \dot{\vec{R}}^2 + \frac{1}{2} m_1 \dot{\vec{r}}_1^2 + \frac{1}{2} m_2 \dot{\vec{r}}_2^2 \end{array}

For the potential energy, we may write:

V=Vi+12ij(Vij+Vji)V = \sum V_i + \frac{1}{2} \sum_{i \neq j} \left ( V_{ij} + V_{ji} \right )

With ViV_i the potential related to the external force on particle ii and VijV_{ij} the potential related to the mutual interaction force from particle ii exerted on particle jj (assuming that all forces are conservative).

8.3Angular Momentum

The total angular momentum is, like the total momentum, defined as the sum of the angular momentum of the two particles:

L=l1+l2=x1×p1+x2×p2\vec{L} = \vec{l}_1 + \vec{l}_2 = \vec{x}_1 \times \vec{p}_1 + \vec{x}_2 \times \vec{p}_2

We can write this in the new coordinates:

L=R×P+r1×p1+r2×p2=Lcm+L\vec{L} = \vec{R} \times \vec{P} + \vec{r}_1 \times \vec{p}_1 + \vec{r}_2 \times \vec{p}_2 = \vec{L}_{cm} + \vec{L}'

We find: that the total angular momentum can be seen as the contribution of the CM and the sum of the angular momentum of the individual particles as seen from the CM.

8.4Reduced Mass

Suppose that there are no external forces. Then the equation of motion for both particles reads as:

m1x1¨=F12m2x2¨=F21=F12\begin{array}{rcl} m_1 \ddot{\vec{x}_1} &= & \vec{F}_{12}\\ m_2 \ddot{\vec{x}_2} &= & \vec{F}_{21} = -\vec{F}_{12} \end{array}

If we divide each equation by the corresponding mass and subtract one from the other we get:

d2dt2(x1x2)=(1m1+1m2)F12\frac{d^2}{dt^2} ( \vec{x}_1 - \vec{x}_2 ) = \left ( \frac{1}{m_1} + \frac{1}{m_2} \right ) \vec{F}_{12}

Note that the interaction force F12\vec{F}_{12} is a function of the relative position of the particles, i.e., x1x2=r1r2\vec{x}_1 - \vec{x}_2 = \vec{r}_1 - \vec{r}_2.

Introduce r12r1r2=x1x2\vec{r}_{12} \equiv \vec{r}_1 - \vec{r}_2 = \vec{x}_1 - \vec{x}_2, then we obtain:

d2dt2r12=(1m1+1m2)F12(r12)\frac{d^2}{dt^2} \vec{r}_{12} = \left ( \frac{1}{m_1} + \frac{1}{m_2} \right ) \vec{F}_{12}(\vec{r}_{12})

As a final step, we introduce the reduced mass μ\mu:

1μ1m1+1m2μ=m1m2m1+m2\frac{1}{\mu} \equiv \frac{1}{m_1} + \frac{1}{m_2} \Leftrightarrow \mu = \frac{m_1 m_2}{m_1 + m_2}

And we can reduced the two-body problem to a single-body problem, by writing down the equation of motion for an imaginary particle with reduced mass.

μd2r12dt2=F12\mu \frac{d^2 \vec{r}_{12}}{dt^2} = \vec{F}_{12}

If m1m2m_1 \gg m_2 we have μm2\mu \rightarrow m_2. This is not surprising: when m1m_1 is much larger than m2m_2, it will look like m1m_1 is not changing its velocity at all. Or seen from the CM: is appears to be not moving. In this case, we can ignore particle 1 and replace it by a force coming out of a fixed position.

8.4.1Back to the Two-Body Problem

Once we solved the problem for the reduced mass, it is straightforward to go back to the two particles. It holds that:

m1r1+m2r2=0m_1 \vec{r}_1 + m_2 \vec{r}_2 = 0
r2=m1m2r1&r2=r1r12\vec{r}_2 = - \frac{m_1}{m_2} \vec{r}_1 \quad\&\quad \vec{r}_2 = \vec{r}_1 - \vec{r}_{12}
r1=m1m1+m2r12r2=m1m1+m2r12\begin{array}{rcl} \vec{r}_1 &= &\frac{m_1}{m_1 + m_2} \vec{r}_{12} \\ \vec{r}_2 &= &-\frac{m_1}{m_1 + m_2} \vec{r}_{12} \end{array}

Thus, if we have solved the motion of the reduced particle, then we can quickly find the motion of the two individual particles (seen from the CM frame).

8.5Kepler Revisited

Kepler revisited.

Figure 3:Kepler revisited.

Now that we have seen how to deal with the two-body problem, we can return to the motion of the Earth around the Sun. This is obviously not a two-body problem, but a many-body problem with many planets.

However, we can approximate it to a two-body problem: we ignore all other planets and leave only the Sun and Earth. Hence, there are no external forces. Consequently, the CM of the Earth-Sun system moves at a constant velocity. And we can take the CM as our origin.

We have to solve the reduced mass problem to find the motion of both the Earth and the Sun:

μd2r12dt2=Gmemsr122r^12\mu \frac{d^2 \vec{r}_{12}}{dt^2} = -\frac{Gm_e m_s}{r_{12}^2} \hat{r}_{12}

Note: this equation is almost identical to the original Kepler problem. All that happened is that mem_e on the left hand side got replaced by μ\mu.

Everything else remains the same: the force is still central and conservative, etc.

8.5.1Where is the CM located?

Position of CM in the sun-earth system.

Figure 4:Position of CM in the sun-earth system.

We can easily find the center of mass of the Earth-Sun system. Chose the origin on the line through the Sun and the Earth (see fig.)


R=msxs+mexems+me=xs+mems+me(xexs)xs+450kmR = \frac{m_s x_s + m_e x_e }{m_s + m_e} = x_s + \frac{m_e}{m_s + m_e} (x_e - x_s)\approx x_s + 450km

In other words: the Sun and Earth rotate in an ellipsoidal trajectory around the center of mass that is 450 km out of the center of the Sun. Compare that to the radius of the Sun itself: Rs=7105R_s = 7 \cdot 10^5 km. No wonder Kepler didn’t notice. The common CM and rotation point is called Barycenter in astronomy.

8.5.2Exoplanets

However, in modern times, this slight motion of stars is a way of trying to find orbiting planets around distant stars. Due to this small ellipsoidal trajectory, sometimes a star moves away from us, and sometimes it comes towards us. This moving away and towards us changes the apparent color of the light emission of molecules or atoms by the Doppler effect. This is a periodic motion, which lasts a ‘year’ of that solar system. Astronomers started looking out for periodic changes in the apparent color of the light of stars. One can also look for periodic changes in the brightness of a star (which is much, much harder than looking at spectral shifts of the light). If a planet is directly between the star and us, the intensity of the starlight decreases a bit. And they found one, and another one, and more and hundreds... Currently, more than 5,000 exoplanets have been found.

with figure from nasa

from nasa

Finding planets via periodic changes in the velocity of a star (from NASA).

Figure 7:Finding planets via periodic changes in the velocity of a star (from NASA).

Finding planets via a periodic change in intensity of a star (from NASA).

Figure 7:Finding planets via a periodic change in intensity of a star (from NASA).

Finding multiple planets via a change in intensity of a star (from NASA).

Finding multiple planets via a change in intensity of a star (from NASA).

8.6Many-Body System

We have seen that we could reduce the two-body problem of sun-earth to a single body question via the concept of reduced mass. But that this strategy does not work for 3, 4, 5, ... bodies.

8.6.1Linear Momentum

We can, however, find some basic features of NN-body problems. In the figure, a collection of NN interacting particles is drawn.

Many particle system.

Figure 10:Many particle system.

Each particle has mass mim_i and is at position xi(t)x_i(t). For each particle, we can set up N2:

mix¨i=Fi,ext+ijFji.m_i \ddot{\vec{x}}_i = \vec{F}_{i, ext} + \sum_{i \neq j} \vec{F}_{ji.}

Summing over all particles and using that all mutual interaction forces form “action = -reaction pairs”, we get:

imix¨i=iFi,extip˙i=iFi,ext\sum_i m_i \ddot{\vec{x}}_i = \sum_i \vec{F}_{i, ext} \Leftrightarrow \sum_i \dot{\vec{p}}_i = \sum_i \vec{F}_{i, ext}

The second part can be written as:

dPdt=iFi,ext with Pipi\frac{d\vec{P}}{dt} = \sum_i \vec{F}_{i, ext} \text{ with } \vec{P} \equiv \sum_i \vec{p}_i

In other words: the total momentum changes due to external forces. If there are no external forces, then the total momentum is conserved. This happens quite a lot actually, if you consider e.g. collisions or scattering.

8.6.2Center of Mass

Analogous to the two-particle case, we see from the total momentum that we can pretend that there is a particle of total mass M=imiM=\sum_i m_i that has momentum P\vec{P}, i.e., it moves at velocity VPM\vec{V} \equiv\frac{\vec{P}}{M} and is located at position:

V=dRdt=midxidtmiR=miximi\vec{V} = \frac{d\vec{R}}{dt} =\frac{\sum m_i \frac{d\vec{x}_i}{dt}}{\sum m_i} \Rightarrow \vec{R} = \frac{\sum m_i \vec{x}_i}{\sum m_i}

Continuing with the analogy, we define relative coordinates:

rixiR\vec{r}_i \equiv \vec{x}_i - \vec{R}

and have a similar rule constraining the relative positions:

miri=0\sum m_i \vec{r}_i = 0

8.6.3Energy

In terms of relative coordinates, we can write the kinetic energy as a part associated with the center of mass and a part that describes the kinetic energy with respect to the center of mass, i.e., ‘an internal kinetic energy’.

Ekin12mivi2=12MR˙2+12mir˙i2=Ekin,cm+Ekin\begin{split} E_{kin} &\equiv \sum \frac{1}{2} m_i v_i^2 \\ &= \frac{1}{2} M \dot{\vec{R}}^2 + \sum \frac{1}{2} m_i \dot{\vec{r}}_i^2 \\ &= E_{kin,cm} + E'_{kin} \end{split}

For the potential energy, we may write:

V=Vi+12ij(Vij+Vji)V = \sum V_i + \frac{1}{2} \sum_{i \neq j} \left ( V_{ij} + V_{ji} \right )

with ViV_i the potential related to the external force on particle ii and VijV_{ij} the potential related to the mutual interaction force from particle ii exerted on particle jj (assuming that all forces are conservative).

8.6.4Angular Momentum

The total angular momentum is, like the total momentum, defined as the sum of the angular momentum of all particles:

L=li=xi×pi\vec{L} = \sum \vec{l}_i = \sum \vec{x}_i \times \vec{p}_i

We can write this in the new coordinates:

L=R×P+ri×pi=Lcm+L\vec{L} = \vec{R} \times \vec{P} + \sum \vec{r}_i \times \vec{p}_i = \vec{L}_{cm} + \vec{L}'

Again, we find that the total angular momentum can be seen as the contribution of the center of mass and the sum of the angular momentum of all individual particles as seen from the center of mass.

The N-body problem is, of course, even more complex than the three-body problem. If we can solve it, it will be under very specific conditions only. However, a numerical approach can be done with great success. Moreover, current computers are so powerful that the system can contain hundred, thousands of particles up to billions depending on the type or particle-particle interaction.

All kind of computational techniques have been developed and various averaging techniques are employed in statistical techniques are introduced from the start. the reason is often, that a particular ‘realisation’ of all positions and velocities of all particles is needed nor sought for. A system is at its macro level described by averaged properties, the exact location of the individual atoms is not needed. You will find applications in cosmology all the way to molecular dynamics, trying to simulate the behavior of proteins or pharmaceuticals.