> How does gravity cause the difference between what the theories predict? AG
I am not sure why you have endless trouble with this. On the Avoid list you repeatedly brought up this question, and in spite of dozens of explanations you raise this question over and over. You need to read a text on this. The old Taylor and Wheeler book on SR gives some reasoning on this. Geroch's book on GR is not too hard to read.LC
On Tuesday, October 13, 2020 at 8:06:30 AM UTC-6, Lawrence Crowell wrote:I am not sure why you have endless trouble with this. On the Avoid list you repeatedly brought up this question, and in spite of dozens of explanations you raise this question over and over. You need to read a text on this. The old Taylor and Wheeler book on SR gives some reasoning on this. Geroch's book on GR is not too hard to read.LCActually, I think your memory is faulty, other than to express your annoyance with my question. In any event, if gravity and acceleration exist for a system under consideration, why is SR relevant? Why does Clark claim that the result of SR must be subtracted for the result of GR to determine an objective outcome, when the conditions of SR are non-existent? AG
> Note that Clark claims SR is irrelevant to the issue of comparing an orbiting clock with a stationary clock on the Earth,
> Sorry, but I don't see [...]
Are you clerking for Barrett? AG
On Tue, Oct 13, 2020 at 1:20 AM Alan Grayson <agrays...@gmail.com> wrote:
> How does gravity cause the difference between what the theories predict? AGThere is no contradiction about what the theories predict because Special Relativity can make no prediction at all about what a clock will do when it is in a gravitational field or is accelerated in any other way; that's why it's called "special", it's only applicable in certain special circumstances. But General Relativity can handle acceleration and gravity. A GPS Satellite is moving fast compared to a clock on the ground so Special Relativity says the clock on the satellite will lose 7210 nanoseconds a day,
but the satellite clock is further from the Earth's center so it's in a weaker gravitational field, and because of that general relatively says the satellite clock will gain 45850 nanoseconds a day relative to the clock on the ground.
So the two theories together predict the satellite clock will gain 45850 −7210 = 38,640 nanoseconds a day relative to a clock on the ground. If this were not taken into account the GPS system would be in error by 6 miles every day and the error would add up, soon the entire GPS system would be useless.
John K Clark
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I will try to give a definitive answer. The Schwarzschild metric is
ds^2 = c^2(1 – 2m/r)dt^2 – (1 – 2m/r)dr^2 – r^2(dθ^2 – sin^2θdφ^2)
for m = GM/c^2. For the motion of a satellite in a circular orbit there is no radial motion so dr = 0. We set this on a plane with θ = π/2 so dθ = 0 and this reduces this to
ds^2 =c^2(1 – 2m/r)dt^2 – r^2dφ^2.
For circular motion dφ/dt = ω and the velocity v = ωr means this is
ds^2 = [c^2(1 – 2m/r) – r^2ω^2]dt^2
and so ds^2 = [c^2(1 – 2m/r) – v^2]dt^2 the term Γ = 1/√[c^2(1 – 2m/r) – v^2] is a general Lorentz gamma factor and in flat space with m = 0 reduces the form we know. ds is an increment in the proper time on the orbiting satellite and t is a coordinate time, say on the ground of the body.
We can do more with this. The ds^2 = [c^2(1 – 2m/r) – r^2dφ^2]dt^2 can be written as
1 = [c^2(1 – 2m/r) – r^2ω^2](dt/ds)^2
Now take a variation on this, where obviously δ1 = 0 and
0 = [c^2δ(1 – 2m/r) – δ(r^2ω^2)](dt/ds)^2 + [c^2(1 – 2m/r) – r^2ω^2]δ(dt/ds)^2.
We think primarily of a variation in the radius and so
0 = -[ 2mc^2/r^2 – 2rω^2](dt/ds)^2δr + [c^2(1 – 2m/r) – r^2ω^2]δ(dt/ds)^2,
where for the time I will ignore the last term. The first term gives
rω^2 = -GM/r,
and this is just Newton’s second law with acceleration a = rω^2 with gravity. Also this is Kepler's third law of planetary motion.
Now I will hand wave a bit here. The term δ(dt/ds)^2 = 1 in the Newtonian limit, but we can feed the general Lorentz gamma factor in that. This will have a correction term to this dynamical equation. This correction is general relativistic. The algebra gets a bit dense, but it is nothing conceptually difficult.
LC
I will try to give a definitive answer. The Schwarzschild metric is
ds^2 = c^2(1 – 2m/r)dt^2 – (1 – 2m/r)dr^2 – r^2(dθ^2 – sin^2θdφ^2)
for m = GM/c^2. For the motion of a satellite in a circular orbit there is no radial motion so dr = 0. We set this on a plane with θ = π/2 so dθ = 0 and this reduces this to
ds^2 =c^2(1 – 2m/r)dt^2 – r^2dφ^2.
For circular motion dφ/dt = ω and the velocity v = ωr means this is
ds^2 = [c^2(1 – 2m/r) – r^2ω^2]dt^2
and so ds^2 = [c^2(1 – 2m/r) – v^2]dt^2 the term Γ = 1/√[c^2(1 – 2m/r) – v^2] is a general Lorentz gamma factor and in flat space with m = 0 reduces the form we know. ds is an increment in the proper time on the orbiting satellite and t is a coordinate time, say on the ground of the body.
We can do more with this. The ds^2 = [c^2(1 – 2m/r) – r^2dφ^2]dt^2 can be written as
1 = [c^2(1 – 2m/r) – r^2ω^2](dt/ds)^2
Now take a variation on this, where obviously δ1 = 0 and
0 = [c^2δ(1 – 2m/r) – δ(r^2ω^2)](dt/ds)^2 + [c^2(1 – 2m/r) – r^2ω^2]δ(dt/ds)^2.
We think primarily of a variation in the radius and so
0 = -[ 2mc^2/r^2 – 2rω^2](dt/ds)^2δr + [c^2(1 – 2m/r) – r^2ω^2]δ(dt/ds)^2,
where for the time I will ignore the last term. The first term gives
rω^2 = -GM/r,
On Tuesday, October 13, 2020 at 3:26:14 PM UTC-5 Lawrence Crowell wrote:I will try to give a definitive answer. The Schwarzschild metric is
ds^2 = c^2(1 – 2m/r)dt^2 – (1 – 2m/r)dr^2 – r^2(dθ^2 – sin^2θdφ^2)
for m = GM/c^2. For the motion of a satellite in a circular orbit there is no radial motion so dr = 0. We set this on a plane with θ = π/2 so dθ = 0 and this reduces this to
ds^2 =c^2(1 – 2m/r)dt^2 – r^2dφ^2.
For circular motion dφ/dt = ω and the velocity v = ωr means this is
ds^2 = [c^2(1 – 2m/r) – r^2ω^2]dt^2
and so ds^2 = [c^2(1 – 2m/r) – v^2]dt^2 the term Γ = 1/√[c^2(1 – 2m/r) – v^2] is a general Lorentz gamma factor and in flat space with m = 0 reduces the form we know. ds is an increment in the proper time on the orbiting satellite and t is a coordinate time, say on the ground of the body.
On Tuesday, October 13, 2020 at 3:28:21 PM UTC-5 Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:26:14 PM UTC-5 Lawrence Crowell wrote:
I will try to give a definitive answer. The Schwarzschild metric is
ds^2 = c^2(1 – 2m/r)dt^2 – (1 – 2m/r)dr^2 – r^2(dθ^2 – sin^2θdφ^2)
for m = GM/c^2. For the motion of a satellite in a circular orbit there is no radial motion so dr = 0. We set this on a plane with θ = π/2 so dθ = 0 and this reduces this to
ds^2 =c^2(1 – 2m/r)dt^2 – r^2dφ^2.
For circular motion dφ/dt = ω and the velocity v = ωr means this is
ds^2 = [c^2(1 – 2m/r) – r^2ω^2]dt^2
and so ds^2 = [c^2(1 – 2m/r) – v^2]dt^2 the term Γ = 1/√[c^2(1 – 2m/r) – v^2] is a general Lorentz gamma factor and in flat space with m = 0 reduces the form we know. ds is an increment in the proper time on the orbiting satellite and t is a coordinate time, say on the ground of the body.
Another erratum. The coordinate time t is for a clock very far removed, not on the ground. On the ground that clock ticks away with a factor Γ = 1/√[c^2 – v^2] change. So there is a relative time difference.
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On 10/13/2020 1:34 PM, Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:28:21 PM UTC-5 Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:26:14 PM UTC-5 Lawrence Crowell wrote:
I will try to give a definitive answer. The Schwarzschild metric is
ds^2 = c^2(1 – 2m/r)dt^2 – (1 – 2m/r)dr^2 – r^2(dθ^2 – sin^2θdφ^2)
for m = GM/c^2. For the motion of a satellite in a circular orbit there is no radial motion so dr = 0. We set this on a plane with θ = π/2 so dθ = 0 and this reduces this to
ds^2 =c^2(1 – 2m/r)dt^2 – r^2dφ^2.
For circular motion dφ/dt = ω and the velocity v = ωr means this is
ds^2 = [c^2(1 – 2m/r) – r^2ω^2]dt^2
and so ds^2 = [c^2(1 – 2m/r) – v^2]dt^2 the term Γ = 1/√[c^2(1 – 2m/r) – v^2] is a general Lorentz gamma factor and in flat space with m = 0 reduces the form we know. ds is an increment in the proper time on the orbiting satellite and t is a coordinate time, say on the ground of the body.
Another erratum. The coordinate time t is for a clock very far removed, not on the ground. On the ground that clock ticks away with a factor Γ = 1/√[c^2 – v^2] change. So there is a relative time difference.A clock on the ground is also moving with rotation of the Earth, with different speed at different latitudes. This is taken out of the equations by comparing the GPS clock to ideal clocks on a fixed (non-rotating Earth) and then after GPS calculates the location on the non-rotating Earth, it calculates what point this is on the rotating Earth.
Brent
On Tuesday, October 13, 2020 at 4:13:05 PM UTC-5 Brent wrote:
On 10/13/2020 1:34 PM, Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:28:21 PM UTC-5 Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:26:14 PM UTC-5 Lawrence Crowell wrote:
I will try to give a definitive answer. The Schwarzschild metric is
ds^2 = c^2(1 – 2m/r)dt^2 – (1 – 2m/r)dr^2 – r^2(dθ^2 – sin^2θdφ^2)
for m = GM/c^2. For the motion of a satellite in a circular orbit there is no radial motion so dr = 0. We set this on a plane with θ = π/2 so dθ = 0 and this reduces this to
ds^2 =c^2(1 – 2m/r)dt^2 – r^2dφ^2.
For circular motion dφ/dt = ω and the velocity v = ωr means this is
ds^2 = [c^2(1 – 2m/r) – r^2ω^2]dt^2
and so ds^2 = [c^2(1 – 2m/r) – v^2]dt^2 the term Γ = 1/√[c^2(1 – 2m/r) – v^2] is a general Lorentz gamma factor and in flat space with m = 0 reduces the form we know. ds is an increment in the proper time on the orbiting satellite and t is a coordinate time, say on the ground of the body.
Another erratum. The coordinate time t is for a clock very far removed, not on the ground. On the ground that clock ticks away with a factor Γ = 1/√[c^2 – v^2] change. So there is a relative time difference.
A clock on the ground is also moving with rotation of the Earth, with different speed at different latitudes. This is taken out of the equations by comparing the GPS clock to ideal clocks on a fixed (non-rotating Earth) and then after GPS calculates the location on the non-rotating Earth, it calculates what point this is on the rotating Earth.
Brent
This gets really complicated. I did a lot of post-Newtonian parameter work on this back in the late 80s. A lot of it was numerical, because on the ground there are different values of gravity, and these too can cause drift. Gravitation, thinking of a Newtonian force, is different near a mountain than on the top of it, and the direction can vary some from the radius. It also fluctuates with tides! The surging in and out of a lot of ocean water actually changes the Newtonian gravitation potential and force.
LC
To view this discussion on the web visit https://groups.google.com/d/msgid/everything-list/ae6a9158-dcf3-4da8-8065-faf236f04210n%40googlegroups.com.
I will try to give a definitive answer.
On 10/13/2020 3:12 PM, Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 4:13:05 PM UTC-5 Brent wrote:
On 10/13/2020 1:34 PM, Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:28:21 PM UTC-5 Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:26:14 PM UTC-5 Lawrence Crowell wrote:
I will try to give a definitive answer. The Schwarzschild metric is
ds^2 = c^2(1 – 2m/r)dt^2 – (1 – 2m/r)dr^2 – r^2(dθ^2 – sin^2θdφ^2)
for m = GM/c^2. For the motion of a satellite in a circular orbit there is no radial motion so dr = 0. We set this on a plane with θ = π/2 so dθ = 0 and this reduces this to
ds^2 =c^2(1 – 2m/r)dt^2 – r^2dφ^2.
For circular motion dφ/dt = ω and the velocity v = ωr means this is
ds^2 = [c^2(1 – 2m/r) – r^2ω^2]dt^2
and so ds^2 = [c^2(1 – 2m/r) – v^2]dt^2 the term Γ = 1/√[c^2(1 – 2m/r) – v^2] is a general Lorentz gamma factor and in flat space with m = 0 reduces the form we know. ds is an increment in the proper time on the orbiting satellite and t is a coordinate time, say on the ground of the body.
Another erratum. The coordinate time t is for a clock very far removed, not on the ground. On the ground that clock ticks away with a factor Γ = 1/√[c^2 – v^2] change. So there is a relative time difference.
A clock on the ground is also moving with rotation of the Earth, with different speed at different latitudes. This is taken out of the equations by comparing the GPS clock to ideal clocks on a fixed (non-rotating Earth) and then after GPS calculates the location on the non-rotating Earth, it calculates what point this is on the rotating Earth.
Brent
This gets really complicated. I did a lot of post-Newtonian parameter work on this back in the late 80s. A lot of it was numerical, because on the ground there are different values of gravity, and these too can cause drift. Gravitation, thinking of a Newtonian force, is different near a mountain than on the top of it, and the direction can vary some from the radius. It also fluctuates with tides! The surging in and out of a lot of ocean water actually changes the Newtonian gravitation potential and force.
LC
And it's further complicated by the Earth being non-spherical. The calculations find the lat/long of a WGS84 ellipsoid. But of course the real Earth isn't exactly an WGS84 ellipsoid either and there have to be local corrections in look-up tables. Off the coast of California where I used to be involved in developing sea-skimming targets the WGS84 "sea level" is about 120ft under water.
Brent
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On Tuesday, October 13, 2020 at 5:16:04 PM UTC-6, Brent wrote:
On 10/13/2020 3:12 PM, Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 4:13:05 PM UTC-5 Brent wrote:
On 10/13/2020 1:34 PM, Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:28:21 PM UTC-5 Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:26:14 PM UTC-5 Lawrence Crowell wrote:
I will try to give a definitive answer. The Schwarzschild metric is
ds^2 = c^2(1 – 2m/r)dt^2 – (1 – 2m/r)dr^2 – r^2(dθ^2 – sin^2θdφ^2)
for m = GM/c^2. For the motion of a satellite in a circular orbit there is no radial motion so dr = 0. We set this on a plane with θ = π/2 so dθ = 0 and this reduces this to
ds^2 =c^2(1 – 2m/r)dt^2 – r^2dφ^2.
For circular motion dφ/dt = ω and the velocity v = ωr means this is
ds^2 = [c^2(1 – 2m/r) – r^2ω^2]dt^2
and so ds^2 = [c^2(1 – 2m/r) – v^2]dt^2 the term Γ = 1/√[c^2(1 – 2m/r) – v^2] is a general Lorentz gamma factor and in flat space with m = 0 reduces the form we know. ds is an increment in the proper time on the orbiting satellite and t is a coordinate time, say on the ground of the body.
Another erratum. The coordinate time t is for a clock very far removed, not on the ground. On the ground that clock ticks away with a factor Γ = 1/√[c^2 – v^2] change. So there is a relative time difference.
A clock on the ground is also moving with rotation of the Earth, with different speed at different latitudes. This is taken out of the equations by comparing the GPS clock to ideal clocks on a fixed (non-rotating Earth) and then after GPS calculates the location on the non-rotating Earth, it calculates what point this is on the rotating Earth.
Brent
This gets really complicated. I did a lot of post-Newtonian parameter work on this back in the late 80s. A lot of it was numerical, because on the ground there are different values of gravity, and these too can cause drift. Gravitation, thinking of a Newtonian force, is different near a mountain than on the top of it, and the direction can vary some from the radius. It also fluctuates with tides! The surging in and out of a lot of ocean water actually changes the Newtonian gravitation potential and force.
LC
And it's further complicated by the Earth being non-spherical. The calculations find the lat/long of a WGS84 ellipsoid. But of course the real Earth isn't exactly an WGS84 ellipsoid either and there have to be local corrections in look-up tables. Off the coast of California where I used to be involved in developing sea-skimming targets the WGS84 "sea level" is about 120ft under water.
Brent
Yes, very complicated to get an exact solution. BUT, what I was trying to say, before getting a ton of crap from LC and Clark, the solution depends ONLY on GR since gravity is involved which distorts the spacetime paths and thus the proper times along these paths. Do you agree with this statement? TIA, AG
To view this discussion on the web visit https://groups.google.com/d/msgid/everything-list/abe62f22-954e-418d-a174-0757c74d4838o%40googlegroups.com.
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On Tuesday, October 13, 2020 at 2:26:14 PM UTC-6, Lawrence Crowell wrote:I will try to give a definitive answer.
So regardless of your subsequent corrections, will you now admit, as I was suggesting, that the exact solution can be determined solely by GR, and that Clark's introducing SR is confusing and mistaken. Thank you in advance for your honesty! AG
On 10/13/2020 3:12 PM, Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 4:13:05 PM UTC-5 Brent wrote:
On 10/13/2020 1:34 PM, Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:28:21 PM UTC-5 Lawrence Crowell wrote:
On Tuesday, October 13, 2020 at 3:26:14 PM UTC-5 Lawrence Crowell wrote:
I will try to give a definitive answer. The Schwarzschild metric is
ds^2 = c^2(1 – 2m/r)dt^2 – (1 – 2m/r)dr^2 – r^2(dθ^2 – sin^2θdφ^2)
for m = GM/c^2. For the motion of a satellite in a circular orbit there is no radial motion so dr = 0. We set this on a plane with θ = π/2 so dθ = 0 and this reduces this to
ds^2 =c^2(1 – 2m/r)dt^2 – r^2dφ^2.
For circular motion dφ/dt = ω and the velocity v = ωr means this is
ds^2 = [c^2(1 – 2m/r) – r^2ω^2]dt^2
and so ds^2 = [c^2(1 – 2m/r) – v^2]dt^2 the term Γ = 1/√[c^2(1 – 2m/r) – v^2] is a general Lorentz gamma factor and in flat space with m = 0 reduces the form we know. ds is an increment in the proper time on the orbiting satellite and t is a coordinate time, say on the ground of the body.
Another erratum. The coordinate time t is for a clock very far removed, not on the ground. On the ground that clock ticks away with a factor Γ = 1/√[c^2 – v^2] change. So there is a relative time difference.
A clock on the ground is also moving with rotation of the Earth, with different speed at different latitudes. This is taken out of the equations by comparing the GPS clock to ideal clocks on a fixed (non-rotating Earth) and then after GPS calculates the location on the non-rotating Earth, it calculates what point this is on the rotating Earth.
Brent
This gets really complicated. I did a lot of post-Newtonian parameter work on this back in the late 80s. A lot of it was numerical, because on the ground there are different values of gravity, and these too can cause drift. Gravitation, thinking of a Newtonian force, is different near a mountain than on the top of it, and the direction can vary some from the radius. It also fluctuates with tides! The surging in and out of a lot of ocean water actually changes the Newtonian gravitation potential and force.
LCAnd it's further complicated by the Earth being non-spherical. The calculations find the lat/long of a WGS84 ellipsoid. But of course the real Earth isn't exactly an WGS84 ellipsoid either and there have to be local corrections in look-up tables. Off the coast of California where I used to be involved in developing sea-skimming targets the WGS84 "sea level" is about 120ft under water.
Brent