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© The scientific sentence. 2010

Relativity: Geodesic equation



1. 4-Vector velocity

Let's consider a particle moving in the space-time coordinate frame. The worldline of the particle is its path function of its proper time as it travels through this space.

The worldline of a moving particle can be written, in its reference frame ax r(τ) = xi(τ), where r(τ) = xi(τ) is its position vector and τ is the proper time (the time in the moving frame).

The particle is being placed in the origin of its frame, so dx = dy = dz = 0, and ds2 = dτ2 (with c = 1).

In the moving frame of the particle: ds = dτ

Now, let's define a 4-Velocity as:
vi = dxi(τ)/dτ = dxi/dτ
In the frame of the moving particle:
vivi = vi gij vj =
gij (dxi/dτ) (dxj/dτ) =
ds2/dτ2 = 1.
The velocity 4-vector is constant.

In the frame of the moving particle:

vi = dxi(τ)/dτ = dxi/dτ

ds = dτ


The velocity 4-vector vi is constant.


2. Geodesic equation

In Euclidean space, straight line is the shortest distance between two points . Curves of minimum length are geodesics.

The geodesic equation is the equation of motion of a freely-falling particle.

The velocity 4-Vector vi = dxi/dτ in the moving frame of the particle is constant, therefore its proper time derivative is zero:

dvi/dτ = d2xi/dτ2 = 0

Geodesic equation:

dvi/dτ = d2xi/dτ2 = 0

We have:

v = gi vi, so
dv = (∂v/∂xj) dxj, then
dv/dτ = (∂v/∂xj) (dxj/dτ)
∂v/∂xj = ∂(gi vi)/∂xj =
gi ∂vi/∂xj + vi ∂gi/∂xj =
gi ∂vi/∂xj + vi Γkijgk =
gk [(gigk-1)∂vi/∂xj + vi Γkij]

We have
gigk-1 = gigk = δik

Therefore:
∂v/∂xj = gk [∂vk/∂xj + vi Γkij]

Hence
dv/dτ = gk [∂vk/∂xj + vi Γkij](dxj/dτ)
= gk [∂vk/∂xj + vi Γkij](dxj/dτ)

We have:
dvk = (∂vk/∂xj)dxj
and
(dxj/dτ) = vj

Therefore
dv/dτ = gk [dvk/dτ + Γkij vi vj]

Hence the geodesic equation is :
[dvk/dτ + Γkij vi vj] = 0

Geodesic equation:

dvk/dτ + Γkijvivj = 0


3. Geodesic equation from Euler-Lagrage equation

The metric is ds² = gμν dxμ dxν.

The path length S is

S = ∫ ds = ∫ [gμν dxμ dxν]¹/2;

Parameterising by λ, the path length S becomes:

S = ∫ ds = ∫ [gμν (dxμ/dλ) (dxν/dλ)]1/2

The Lagrangian is L = ds/dλ = [gμν (dxμ/λ) (dxν/λ)]1/2

Euler-Lagrange equation to use is:

∂L/∂xα = d(∂L/∂x'α)/dλ

L does not depend partially on λ, so instead of using L = [gμν (dxμλ) (dxν/λ ]1/2, we use L² = gμν (dxμλ) (dxν/λ) . It leads to the same equation.

∂L²/∂xα = d(∂L²/∂x'α)/dλ

The derivative gives:

2L∂L/∂xα - d(2L∂L/∂x'α)/d&lambda} = 0 or
2L{∂L/∂xα - d(∂L/∂x'α)/dλ} = 0

That is

∂L/∂xα - d(∂L/∂x'α)/dλ = 0

With

x'μ = d xμ/dλ

1.First term:

∂L/∂xα = ∂[gμν (dx'μ) (dx'ν)]/∂xμ = dx'μ dx'ν ∂gμν/∂xα

2. Second term:

d(∂L/∂x'α)/dλ

2.1.

∂L/∂x'α = ∂[gμν (dx'μ) (dx'ν)]/∂x'α

We have:

∂ dx'μ/∂ dx'ν = δ(μν).
So d(∂L/∂x'α)/dλ= gαν (dx'ν) + gμα (dx'μ)

2.2

d(∂L/∂x'α)/dλ

We have

∂gαν/dλ = (∂gαν/∂xβ) (dxβ/dλ)

Therefore

d(∂L/∂x'α)/dλ = (∂gαμ/∂xβ)(dxβ/dλ) dx'μ + (∂gαν/xβ)(dxβ/dλ) dx'ν + gαν (dx'ν/dλ) + gμα (dx'μ/dλ)
= (∂gαμ/∂xβ)(x'β) dx'μ + (∂gαν/xβ)(x'β) dx'ν + gαν (x''ν) + gμα (x''μ)

The two last terms are the same, so
d(∂L/∂x'α)/dλ =
(∂gαμ/∂xβ)(x'β) dx'μ + (∂gαν/xβ)(x'β) dx'ν + 2gαν (x''ν)

3.Euler-Lagrange equation :

dx'μ dx'ν ∂gμν/∂xα =
(∂gαμ/∂xβ)(x'β) dx'μ + (∂gαν/xβ)(x'β) dx'ν + 2gαν (x''ν)

or

2gαν (x''ν) = dx'μ dx'ν ∂gμν/∂xα - (∂gαμ/∂xβ)(x'β) dx'μ - (∂gαν/xβ)(x'β) dx'ν

Multiplying the two hands of this equation by (1/2)gασ , we get by changing β in ν into the second term and β into μ in the third term:

x''σ = (1/2)gασ { dx'μ dx'ν ∂gμν/∂xα - (∂gαμ/∂xν)(x'ν) dx'μ - (∂gαν/xμ)(x'μ) dx'ν } =
(1/2)gασ { ∂gμν/∂xα - ∂gαμ/∂xν - ∂gαν/xμ }dx'μ dx'ν

Or

x''σ + (1/2)gασ { - ∂gμν/∂xα + ∂gαμ/∂xν + ∂gαν/xμ }dx'μ dx'ν = 0

We have the following Christoffel symbol:

Γσμν = (1/2)gασ { ∂gαμ/∂xν + ∂gαν/xμ - ∂gμν/∂xα }

That is

x''σ + Γσ μν x'μ x'ν = o

x''σ + Γσμν x'μ x'ν = 0

Which is the geodesic equation.




  


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