vanesch
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hossi said:By globally I always mean on the entire manifold. I guess we have some disagreement on the equivalence principle. As I understand it it says: the local effects of gravity in curved space are identical to those that an uniformly accelerated observer in globally flat space experiences.
Yes, which comes down to saying that the effects of gravity (the kinematical effects: we're only concerned with test particles here, not with experiments where the dynamics of gravity enters into account (where the test masses MODIFY the metric or something else) are solely dependent on the metric on a local, finite patch around where we try to establish them.
The uniformly accelerated observer in globally flat space is your Rindler observer. Now you have two of them, with positive or negative acceleration.
Eh, no. I only have one of them: it is my right to consider one, or the other and that choice is set up by the experimental situation. I mean: in a rocket, there are not TWO but only ONE coordinate system which is "fixed to the rocket", and in this system of coordinates, the acceleration is well-defined: it is defined by the behavior of NORMAL particles (of which the experimental existence doesn't need any explanation).
With these normal particles, in this rocket frame (X,Y,Z,T) we can establish the local metric, and it is the Rindler metric, and the sign of the acceleration in this metric is unambiguously established. In fact, it is established by "letting the particles fall" in this rocket frame. They will "fall down" (in the rocket frame = Rindler metric) in the sense that their equation of motion will be something of the kind: Z(T) = Z0 + V0 T - a/2 T^2 (Newtonian approximation). These are the geodesics of the Rindler metric. These same geodesics (world lines) are of course straight lines because when we transform this to the Lorentz frame, we have free particles in flat space. Now, this transformation between the Lorentz frame and the rocket frame is a transformation of coordinates on the manifold, and one doesn't have any choice there in the sign of the acceleration.
And if a-particles 1) describe a world line and 2) follows uniform motion in the Lorentz frame, then its world lines, are geodesics and hence will remain geodesics of the Rindler metric in the X,Y,Z,T coordinate system.
If you insist that in the coordinate frame XYZ,T (fixed to the rocket, so experimentally entirely unambiguous), the equation of motion of an a-particle is not a geodesic Z(T) = Z0 + V0 T - a/2 T^2, but rather
Z(T) = Z0 + V0 T PLUS a/2 T^2, then the only possibilities are:
a) that this equation of motion does not describe a world line but is observer-dependent OR
b) that the equation of motion in the Lorentz frame is NOT uniform motion.
The reason is of course that a world line cannot be a geodesic of a metric in one coordinate system and NOT be a geodesic in another coordinate system (a geodesic is a concept that is coordinate-system independent).
Now, both claims are denied by you, so this cannot be true.
Hence, the only possible motion for an a-particle, in the rocket frame, is given by Z(T) = Z0 + V0 T - a/2 T^2 (= a geodesic of the metric), which can be called "falling down in the rocket".
Since space is globally flat for the accelerated observer, you can of course then say, well, then it's the same everywhere and I only look at a local piece again. That I think, is what you are doing (?). But that doesn't change the fact that the space for the Rindler observer is globally flat, and, in particular, if this observer is uniformly accelerated, he doesn't move on a geodesic.
Yes, but an *observer* doesn't have to move on a geodesic! An "observer" is a coordinate system, meaning: mapping 4 numbers on a patch of spacetime. That's the whole idea of coordinate systems on a manifold.
The Rindler space is flat and therefore the particle, no matter which, does not 'fall' at all.
Well, it "falls" of course from the POV of the coordinate system of the rocket (with the Rindler metric), where the equation of motion is:
Z(T) = Z0 + V0 T - a/2 T^2 (in the Newtonian limit)
which is the equation of motion of a "falling" particle.
You are repeating your mistake. I have the same metric over a local patch. In the one case, I attribute it (using the equivalence principle) to an Rindler observer (I am trying to use your reasoning) with positive acceleration, in the other case with negative acceleration.
You can't. In a GIVEN coordinate system, (such as the one in a rocket), the acceleration is unambiguously defined. You cannot assign TWO accelerations to it. The unambiguously defined acceleration defines the sign of the acceleration in the metric expressed in this ONE AND UNIQUE coordinate system, which is nothing else but a Rindler metric. There's no way to assign TWO DIFFERENT accelerations to the same coordinate system, because the transformation between this coordinate system (of the rocket) and a given Lorentz frame is UNIQUELY DEFINED. It is a *coordinate transformation*. X,Y,Z and T are FUNCTIONS of (x,y,z,t) in a unique way.
The prescription you need to 'simulate' gravitational effects in flat space is different for both particles.
But as I outlined above, there is only ONE way to be compatible with:
a) a-particles describe world lines (coordinate-independent)
b) a-particles describe geodesics in the Lorentz frame.
If the world lines are geodesics of the metric in ONE frame, they are geodesics in ALL frames, because "geodesic" and "world line" are geometric concepts which are coordinate independent.
It's not a global coordinate system, therefore you can't just take the coefficients in ds^2 and say, it's a metric of the manifold. Look, if spacetime is flat, you can accelerate your observer as you like, it better stays flat.
Of course. The Rindler metric is a flat metric, but it is not Lorentzian. It isn't "global" because some piece of spacetime is missing, but it surely is "global enough" to define the metric over a finite local patch. (and not just in one point). By the equivalence principle, on which we both seem to agree, this should be good enough to determine uniquely the equation of motion in it.
You can of course use local coordinates like the ones you use, but you have to be careful what conclusions you draw from the coefficients, that was all I wanted to say.
But "local coordinates over a finite patch of spacetime" is all you have in GR. You have to be able to deduce everything from within local coordinates and the metric expressed in it. It's the essence of the equivalence principle. And what I'm saying is that these local coordinates are THE SAME for an observer on the surface of the earth, and in an accelerated rocket (up to tiny tidal effects).
If these are the same, then the equation of motion that you can derive of it, should be the same. And you claim it doesn't.
I have worked out the definitions in your paper and came to the conclusions mentioned previously ! You first publish (miracles happen every day still), then you claim that you did not check things yet but at the same time you are telling to everyone who is kindly trying to inform you that the miracle does not happen that it somehow HAS to occur. As far as I can guess your notion of transpose : E_\mu E^T_\nu = g_\mu \nu (I remind you : I asked you to clarify this issue in the beginning), so there you have it.