Given a DeSitter-space metric from the line element:
ds2=(1−r2R2)dt2−(1−r2R2)−1dr2−r2dΩ2
Where R=√3Λ, and Λ is a positive cosmological constant, I am trying to derive the equations for radial null geodesics. I derived the geodesic equations from the definition and Christoffel symbols, but I'm a little suspicious of my solution to these equations. So, the differential equations I derived are (λ is an "affine" parameter):
d2rdλ2−rR2(1−r2R2)(dtdλ)2+rR2−r2(drdλ)2=0
d2tdλ2+2rr2−R2dtdλdrdλ=0
Now, I tried to use the identity u⋅u=0 where u is the four velocity (or I guess a vector tangent to the light ray's world line if I'm thinking about this correctly). Thus, because u2=u3=0:
gμνuμuν=(1−r2R2)(u0)2−(1−r2R2)−1(u1)2=0
⟹−rR2(1−r2R2)(u0)2+rR2−r2(u1)2=0
Then, substituting this into the first (radial) geodesic equation, I get:
d2rdλ2=0
This is what I am suspicious of. It seems too easy and simple. Do you think this is correct? If I carry on anyways and integrate to find u0(r) then substitute r(λ) I get the following for t(λ):
r(λ)=Aλ+B
t(λ)=DARtanh−1[Aλ+BR]+E
Where, A,B,D,E are constants of integration. To sum up, is this a viable way to solve these equations or am I missing something? If this is correct, how does one define initial conditions for these solutions. Specifically, the derivative conditions t′(0) and r′(0).
This post imported from StackExchange Physics at 2014-08-09 08:48 (UCT), posted by SE-user TylerHG