From: Androcles on

"Simp" <alsor(a)interia.pl> wrote in message
news:b68553e2-2878-44fe-9cb4-8e889eab075b(a)d37g2000yqm.googlegroups.com...
| On 5 Lip, 09:53, "Androcles" <Headmas...(a)Hogwarts.physics_z> wrote:
|
| > Kepler (two body, no one):
| > T(m) = 2pi sqrt(a^3/G(M+m));
| > =======================
| > Elliptical orbits are not 2pi in length.
| > DOA.
|
| 2pi is angle - full cycle, closed loop...
|

Precession is more than 2pi radians from aphelion to aphelion.
Even then one needs Newton's absolute coordinate frame of
reference that he called the "fixed" stars, there being no other
reference available, and we need to take into account Earth's
precession.

From: J. Clarke on
On 7/5/2010 9:41 AM, Simp wrote:
> On 5 Lip, 15:19, Simp<al...(a)interia.pl> wrote:
>> On 5 Lip, 04:38, "J. Clarke"<jclarke.use...(a)cox.net> wrote:
>>
>>>> Anomalous orbit precession?
>>>> Only optical effect - illusion
>>>> (true sun position is delayed in time, more than mercury).
>>
>>> You don't seem to understand the difference between period and precession.
>>
>
>> Precession is ~560 arcsec / year...
>> it's little more than 0.4 arcsec.
>
> 56 / year = 5600 / 100y
>
> 5599.7 / 100y - Observed;
> 100% Jupiter.

So why doesn't the calculation method that successfully accounts for
Jupiter in the analysis of the orbits of the other planets work for
Mercury?

From: Simp on
On 5 Lip, 15:44, "Androcles" <Headmas...(a)Hogwarts.physics_z> wrote:
> "Simp" <al...(a)interia.pl> wrote in message
>
> news:b68553e2-2878-44fe-9cb4-8e889eab075b(a)d37g2000yqm.googlegroups.com...
> | On 5 Lip, 09:53, "Androcles" <Headmas...(a)Hogwarts.physics_z> wrote:
> |
> | > Kepler (two body, no one):
> | > T(m) = 2pi sqrt(a^3/G(M+m));
> | > =======================
> | > Elliptical orbits are not 2pi in length.
> | > DOA.
> |
> | 2pi is angle - full cycle, closed loop...
> |
>
> Precession is more than 2pi radians from aphelion to aphelion.
> Even then one needs Newton's absolute coordinate frame of
> reference that he called the "fixed" stars, there being no other
> reference available, and we need to take into account Earth's
> precession.

T is for 2pi radians only.
(v/c)^2 - delay, light aberration, ect.

a = 1.75 arcsecs - deflection angle.
1.75 / 3600 / 360 = (v/c)^2;
v = 350 km/s - CMB radiation.
v - average star-sun velocity.

Shapiro - (v/c)^2;
simple Sagnac effect.
From: Androcles on

"Simp" <alsor(a)interia.pl> wrote in message
news:4c9f6f68-624e-4de0-bb0a-9f57a818e1fa(a)z8g2000yqz.googlegroups.com...
| On 5 Lip, 15:44, "Androcles" <Headmas...(a)Hogwarts.physics_z> wrote:
| > "Simp" <al...(a)interia.pl> wrote in message
| >
| >
news:b68553e2-2878-44fe-9cb4-8e889eab075b(a)d37g2000yqm.googlegroups.com...
| > | On 5 Lip, 09:53, "Androcles" <Headmas...(a)Hogwarts.physics_z> wrote:
| > |
| > | > Kepler (two body, no one):
| > | > T(m) = 2pi sqrt(a^3/G(M+m));
| > | > =======================
| > | > Elliptical orbits are not 2pi in length.
| > | > DOA.
| > |
| > | 2pi is angle - full cycle, closed loop...
| > |
| >
| > Precession is more than 2pi radians from aphelion to aphelion.
| > Even then one needs Newton's absolute coordinate frame of
| > reference that he called the "fixed" stars, there being no other
| > reference available, and we need to take into account Earth's
| > precession.
|
| T is for 2pi radians only.

So it's only an approximation.


| (v/c)^2 - delay, light aberration, ect.
|
| a = 1.75 arcsecs - deflection angle.
| 1.75 / 3600 / 360 = (v/c)^2;
| v = 350 km/s - CMB radiation.
| v - average star-sun velocity.
|
| Shapiro - (v/c)^2;
| simple Sagnac effect.

http://www.androcles01.pwp.blueyonder.co.uk/Shapiro/Crapiro.htm
Simple Sagnac effect = simple Coriolis effect.
http://ww2010.atmos.uiuc.edu/(Gh)/guides/mtr/fw/gifs/coriolis.mov


From: Simp on
On 5 Lip, 17:29, "Androcles" <Headmas...(a)Hogwarts.physics_z> wrote:
> "Simp" <al...(a)interia.pl> wrote in message
>
> news:4c9f6f68-624e-4de0-bb0a-9f57a818e1fa(a)z8g2000yqz.googlegroups.com...
> | On 5 Lip, 15:44, "Androcles" <Headmas...(a)Hogwarts.physics_z> wrote:
> | > "Simp" <al...(a)interia.pl> wrote in message
> | >
> | >news:b68553e2-2878-44fe-9cb4-8e889eab075b(a)d37g2000yqm.googlegroups.com....
> | > | On 5 Lip, 09:53, "Androcles" <Headmas...(a)Hogwarts.physics_z> wrote:
> | > |
> | > | > Kepler (two body, no one):
> | > | > T(m) = 2pi sqrt(a^3/G(M+m));
> | > | > =======================
> | > | > Elliptical orbits are not 2pi in length.
> | > | > DOA.
> | > |
> | > | 2pi is angle - full cycle, closed loop...
> | > |
> | >
> | > Precession is more than 2pi radians from aphelion to aphelion.
> | > Even then one needs Newton's absolute coordinate frame of
> | > reference that he called the "fixed" stars, there being no other
> | > reference available, and we need to take into account Earth's
> | > precession.
> |
> | T is for 2pi radians only.
>
> So it's only an approximation.
>
> | (v/c)^2 - delay, light aberration, ect.
> |
> | a = 1.75 arcsecs - deflection angle.
> | 1.75 / 3600 / 360 = (v/c)^2;
> | v = 350 km/s - CMB radiation.
> | v - average star-sun velocity.
> |
> | Shapiro - (v/c)^2;
> | simple Sagnac effect.
>
>  http://www.androcles01.pwp.blueyonder.co.uk/Shapiro/Crapiro.htm
> Simple Sagnac effect = simple Coriolis effect.
>    http://ww2010.atmos.uiuc.edu/(Gh)/guides/mtr/fw/gifs/coriolis.mov

Yes, but we don't see light in fly.

T1 = d(t=0)/c, light speed on Mars is c;
and back:
T2 = d(t=T1)/c; light speed on Earth is c;

======
v = 350 km/s - solar wind speed, not stars.