Alternative Splash image; Double Star orbits
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Further thought:
what I could easily do for each binary in the 6th catalog via Perl, Kepler's 3rd law above and the respective colors from 'stars.txt' (Hipparcos data), would be a plot of the Primary color versus m1+m2, the sum of masses of the binary system.
If we see some color--mass correlation, we could exploit it...
Bye Fridger
what I could easily do for each binary in the 6th catalog via Perl, Kepler's 3rd law above and the respective colors from 'stars.txt' (Hipparcos data), would be a plot of the Primary color versus m1+m2, the sum of masses of the binary system.
If we see some color--mass correlation, we could exploit it...
Bye Fridger
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My only additional thought when I was looking at this was that, since the 6th catalog lists the WDS coordinates for every pair, it would be possible to extract secondary spectral types when these are listed in WDS. Unfortunately, it appeared that barely one in 50 WDS entries contained a second spectral type, and that was presented in no standard format I could discern.
Grant
Grant
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t00fri wrote:If we see some color--mass correlation, we could exploit it...
There's obviously a colour-mass correlation.
Since you seem to be ignoring me unless I'm "useful" , here you go - this is the ZAMS for stars with z=0.001 and for z=0.020 from the Geneva Evolution files. (my spectral types may be incorrect because I can't find a single agreed-on list of spectral type vs temperature, but the temperatures are right as read from the files).
I can't get the formatting straight here, but if you copy and paste into a text file it should be more obviousl But again, this is only the Zero Age Main Sequence for these stars, and doesn't say anything about what they evolve into.
Code: Select all
Age M Log T Log L T/K Ls Ts Rs R/AU Spec Type
lots 0.09 3.430 -4.6 2692 0.00003 2691.53 0.1015 0.0005 M5 VI
lots 0.1 3.504 -3.5 3192 0.00032 3191.54 0.11 0.0005 M2 VI
lots 0.2 3.557 -2.20 3606 0.00631 3605.79 0.195 0.0009 K9 VI
lots 0.3 3.585 -1.78 3846 0.017 3845.92 0.28 0.0013 K8 VI
1.62E+09 0.4 3.619 -1.484 4159 0.033 4159.11 0.365 0.0017 K6 VI
7.94E+08 0.5 3.641 -1.2 4375 0.063 4375.22 0.45 0.0021 K4 VI
4.53E+08 0.6 3.686 -0.863 4853 0.137 4852.89 0.535 0.0025 K1 VI
2.54E+08 0.7 3.737 -0.546 5458 0.28 5457.58 0.62 0.0029 G5 VI
9.00E+07 0.8 3.77 -0.3 5888 0.50 5888.44 0.705 0.0033 G1 VI
4.00E+07 0.9 3.801 -0.062 6324 0.87 6324.12 0.79 0.0037 F8 VI
4.00E+07 1 3.828 0.153 6730 1.42 6729.77 0.875 0.0041 F5 VI
4.00E+07 1.25 3.91 0.592 8128 3.91 8128.31 1.00 0.0046 A8 VI
8.51E+07 1.5 3.986 0.932 9683 8.55 9682.78 1.04 0.0048 A4 VI
8.68E+07 1.7 4.034 1.157 10814 14.35 10814.34 1.08 0.0050 A0 VI
1.90E+07 2 4.086 1.411 12190 25.76 12189.90 1.14 0.0053 B9 VI
1.48E+07 2.5 4.151 1.773 14158 59.29 14157.94 1.28 0.0059 B8 VI
1.19E+06 3 4.207 2.057 16106 114.02 16106.46 1.37 0.0064 B6 VI
1.00E+06 4 4.276 2.492 18880 310.46 18879.91 1.65 0.0077 B4 VI
1.17E+06 5 4.325 2.817 21135 656.15 21134.89 1.91 0.0089 B3 VI
Age M Log T Log L T/K Ls Ts Rs R/AU Spec Type
(BD) 0.07 3.340 -5.00 2188 0.00001 2187.76 0.1095 0.0005 M8 V
Proxima 0.1 3.430 -4.30 2692 0.00005 2691.53 0.135 0.0006 M5 V
Barnard 0.2 3.482 -3.40 3034 0.0004 3033.89 0.22 0.0010 M4 V
Gliese 876 0.3 3.544 -2.00 3499 0.0100 3499.45 0.305 0.0014 M0 V
4.30E+08 0.4 3.572 -1.64 3733 0.0229 3732.50 0.39 0.0018 K8 V
8.13E+08 0.5 3.595 -1.37 3936 0.0427 3935.50 0.475 0.0022 K7 V
5.28E+08 0.6 3.623 -1.09 4198 0.0813 4197.59 0.56 0.0026 K5 V
3.36E+08 0.7 3.654 -0.821 4508 0.1510 4508.17 0.645 0.0030 K3 V
1.27E+09 0.8 3.692 -0.576 4920 0.27 4920.40 0.73 0.0034 K1 V
1.00E+08 0.9 3.724 -0.352 5297 0.44 5296.63 0.815 0.0038 G7 V
5.00E+07 1 3.755 -0.132 5689 0.74 5688.53 0.9 0.0042 G3 V
3.30E+08 1.25 3.811 0.367 6471 2.33 6471.43 1.22 0.0056 F7 V
6.00E+07 1.5 3.862 0.711 7278 5.14 7277.80 1.43 0.0066 F1 V
8.51E+07 1.7 3.911 0.949 8147 8.89 8147.04 1.50 0.0070 A8 V
1.10E+07 2 3.958 1.209 9078 16.18 9078.21 1.63 0.0076 A5 V
7.00E+06 2.5 4.031 1.6 10740 39.81 10739.89 1.83 0.0085 A0 V
2.36E+06 3 4.088 1.909 12246 81.10 12246.16 2.00 0.0093 B9 V
1.00E+06 4 4.173 2.385 14894 242.66 14893.61 2.34 0.0109 B7 V
1.00E+06 5 4.235 2.74 17179 549.54 17179.08 2.65 0.0123 B6.5 V
(the star's mass is in the second column). The "age" is just the age (in years) at which the grid starts, usually assumed to be when the star forms - if it's a few billion years then you can assume that the star is like that up til that time). Ls, and Rs are luminosity in Sols, and Radius in Sols.
Last edited by Evil Dr Ganymede on 13.10.2004, 00:11, edited 1 time in total.
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granthutchison wrote:My only additional thought when I was looking at this was that, since the 6th catalog lists the WDS coordinates for every pair, it would be possible to extract secondary spectral types when these are listed in WDS. Unfortunately, it appeared that barely one in 50 WDS entries contained a second spectral type, and that was presented in no standard format I could discern.
Grant
Grant,
funny coincidence...
just at this same time I happened to investigate the same issue . For my modem the download of the WDS takes too long, but I still have the XEphem converted results from the WDS. It seemed to me from there that there should be quite many systems with both color classes specified. But you certainly had a more direct view.
Bye Fridger
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Evil Dr Ganymede wrote:t00fri wrote:If we see some color--mass correlation, we could exploit it...
There's obviously a colour-mass correlation.
..
- this is the ZAMS for stars with z=0.001 and for z=0.020 from the Geneva Evolution files. (my spectral types may be incorrect because I can't find a single agreed-on list of spectral type vs temperature, but the temperatures are right as read from the files).
I can't get the formatting straight here, but if you copy and paste into a text file it should be more obviousl But again, this is only the Zero Age Main Sequence for these stars, and doesn't say anything about what they evolve into.
....
(the star's mass is in the second column). The "age" is just the age (in years) at which the grid starts, usually assumed to be when the star forms - if it's a few billion years then you can assume that the star is like that up til that time). Ls, and Rs are luminosity in Sols, and Radius in Sols.
Evil Dr.
This looks like worth a try.
I should just understand a little better. Can you point me to the original file and remind me what the Geneva Evolution files are precisely? Now this is only a small sample of stars ; how exactly was it selected apart from the z-window? What is of particular interest is the spread in the temperature-mass correlation, in order to arrive at a feel for the uncertainties involved in this method.
Once we have some reasonably sensible correlation of
color/temperature versus mass, we could inject the estimate of the primary mass from the quoted color information in the Hipparcos data (stars.txt) for our binaries and try to get hold of the seconday mass from knowing m1+m2.
In some prominent cases one could cross check the results against the published individual masses.
Very interesting...
Bye Fridger
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Here are the grids of which I speak:
http://obswww.unige.ch/~mowlavi/evol/stev_database.html
Click on the links there and you'll get to loads of evolutionary tables for different masses and metallicities.
The masses from 0.8 Sols and up are provided in the tables there... I can't recall where I found the ones below that, I think I got those from data on stars of those masses and generalising somewhat.
The uncertainties are probably huge, to be honest. This is all what theory suggests, not what is actually out there (which is complicated by all sorts of things like compositional differences and just being randomly awkward) - so you should probably think of them more as guidelines.
http://obswww.unige.ch/~mowlavi/evol/stev_database.html
Click on the links there and you'll get to loads of evolutionary tables for different masses and metallicities.
The masses from 0.8 Sols and up are provided in the tables there... I can't recall where I found the ones below that, I think I got those from data on stars of those masses and generalising somewhat.
The uncertainties are probably huge, to be honest. This is all what theory suggests, not what is actually out there (which is complicated by all sorts of things like compositional differences and just being randomly awkward) - so you should probably think of them more as guidelines.
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Grant and friends,
... exploiting a bit my vacations, I spent several hours today reading in various relevant books I happen to have in my bookshelf. I think I understood a number of things now that bugged me previously:
Here we go:
One typically may consider 3 coordinate systems for our problem of binary orbits:
i) Observer at rest (i.e. at the coordinate origin). In this frame the barycenter moves linearly with time
ii) Barycenter at rest, i.e. x_b(t) = 0, observer is comoving. Here we have
iii) Primary at rest, the system that is used in all
practical observations! (observer comoving)
It was my impression that some of the previous discussions mixed these systems implicitly or explicitly up.
Clearly all quoted orbital elements in catalogs for visual binaries refer to system iii) where the primary is at rest.
Next let me remember,
Why we need exactly 6 orbital elements to characterize the secondarie's orbit in 3d space?
From what observations are these 6 parameters derived in practice!?
(answer):
a) simplest and approach
---------------------------------------
In the limit that only the gravitational force of the primary is considered ( m2/m1 -> 0),
the secondary's orbit arises --after reduction of the 2-body problem to an effective 1-body problem --in terms of the difference vector x(t) as solution of the equation of motion.
The latter is a second order differential equation that we all know and love . To make this initial value problem unique, we have to prescribe at initial epoch t0 both x(t0) and dx(t0)/d t =v(t0), the initial velocity of the secondary.
In 3d space the initial position x(t0) and velocity v(t0) of the secondary in frame iii) precisely comprise 6 independent parameters, directly accessible through binary star observations.
It is a simple but instructive exercise of celestial mechanics to relate these 6 initial values to the standard 6 orbital elements (P,e,i,Omega,w, Periheltime) in a convenient frame
The assumption of a non-vanishing m2/m1 ratio will lead to the so-called "osculating elements" for which m2/m1 needs to be known. Let me turn to this case next:
=========>
b) In reality a nonvanishing secondary mass causes also a gravitational field that feeds back onto the primary. Yet one may take account of this by rescaling the initial data simply as follows:
replace the gravitational constant
in the equations of motions and modify the initial data by
Obviously, the new determination of the orbital elements
now requires also as 7th parameter m2/m1 as input. I have done all those calculations today.
The net effect is that in the orbital elements i,Omega,w
the m2/m1 cancels out, while in the conic section (ellipse) parameters the m2/m1 dependence appears in consistency with the 3rd Kepler law and the barycenter rule.
I hope this clears up some issues.
Bye Fridger
... exploiting a bit my vacations, I spent several hours today reading in various relevant books I happen to have in my bookshelf. I think I understood a number of things now that bugged me previously:
Here we go:
One typically may consider 3 coordinate systems for our problem of binary orbits:
i) Observer at rest (i.e. at the coordinate origin). In this frame the barycenter moves linearly with time
Code: Select all
x_b(t) = a t + b ; (x_b, x_1, x_2, a,b are all vectors)
x_1(t) = x_b(t) - m2/(m1+m2) x(t)
x_2(t) = x_b(t) + m1/(m1+m2) x(t)
x(t) = x_2(t) - x_1(t)
ii) Barycenter at rest, i.e. x_b(t) = 0, observer is comoving. Here we have
Code: Select all
x_b(t) = 0
x_1(t) = - m2/(m1+m2) x(t)
x_2(t) = m1/(m1+m2) x(t)
x(t) = x_2 (t) - x_1(t)
|x_1/x_2| = m2/m1
iii) Primary at rest, the system that is used in all
practical observations! (observer comoving)
Code: Select all
x_1(t) = 0
x_2(t) = x(t)
x_b(t) = m2/(m1+m2) x(t)
It was my impression that some of the previous discussions mixed these systems implicitly or explicitly up.
Clearly all quoted orbital elements in catalogs for visual binaries refer to system iii) where the primary is at rest.
Next let me remember,
Why we need exactly 6 orbital elements to characterize the secondarie's orbit in 3d space?
From what observations are these 6 parameters derived in practice!?
(answer):
a) simplest and approach
---------------------------------------
In the limit that only the gravitational force of the primary is considered ( m2/m1 -> 0),
the secondary's orbit arises --after reduction of the 2-body problem to an effective 1-body problem --in terms of the difference vector x(t) as solution of the equation of motion.
The latter is a second order differential equation that we all know and love . To make this initial value problem unique, we have to prescribe at initial epoch t0 both x(t0) and dx(t0)/d t =v(t0), the initial velocity of the secondary.
In 3d space the initial position x(t0) and velocity v(t0) of the secondary in frame iii) precisely comprise 6 independent parameters, directly accessible through binary star observations.
It is a simple but instructive exercise of celestial mechanics to relate these 6 initial values to the standard 6 orbital elements (P,e,i,Omega,w, Periheltime) in a convenient frame
The assumption of a non-vanishing m2/m1 ratio will lead to the so-called "osculating elements" for which m2/m1 needs to be known. Let me turn to this case next:
=========>
b) In reality a nonvanishing secondary mass causes also a gravitational field that feeds back onto the primary. Yet one may take account of this by rescaling the initial data simply as follows:
replace the gravitational constant
Code: Select all
G^2 -> G^2*(1 + m2/m1)
in the equations of motions and modify the initial data by
Code: Select all
x(t0)
v(t0)/G -> v(t0)/(G*sqrt(1+m2/m1))
Obviously, the new determination of the orbital elements
now requires also as 7th parameter m2/m1 as input. I have done all those calculations today.
The net effect is that in the orbital elements i,Omega,w
the m2/m1 cancels out, while in the conic section (ellipse) parameters the m2/m1 dependence appears in consistency with the 3rd Kepler law and the barycenter rule.
I hope this clears up some issues.
Bye Fridger
Last edited by t00fri on 13.10.2004, 17:31, edited 2 times in total.
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granthutchison wrote:I'm not seeing it, I'm afraid.
The derived conic section surely applies independently of the position of the barycentre, with only a necessary change in the radius of gyration of each body. The body-centred and barycentric elements are otherwise identical.
Are we using different assumptions on how these orbits were derived?
I'm assuming that a Keplerian fit is made to the observed change in angular separation and position angle against time. The shape and orientation of an orbit derived in this way is independent of the barycentre position.
Are you starting from the same place?
Grant
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granthutchison wrote:I'm not seeing it, I'm afraid.
The derived conic section surely applies independently of the position of the barycentre, with only a necessary change in the radius of gyration of each body. The body-centred and barycentric elements are otherwise identical.
Grant
Grant,
too bad, you are (mostly?) right, of course.
I was too inpatient , as to my conclusions:
since I calculated in units m1=1, I had overlooked another m-dependence after (too quickly ) rescaling back to general m1. So after correction of this blunder, we seem to be back at the old story.
So I'll edit my above post accordingly, in order to avoid further confusion.
Bye Fridger
Last edited by t00fri on 13.10.2004, 18:08, edited 1 time in total.
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granthutchison wrote:Are we using different assumptions on how these orbits were derived?granthutchison wrote:I'm not seeing it, I'm afraid.
The derived conic section surely applies independently of the position of the barycentre, with only a necessary change in the radius of gyration of each body. The body-centred and barycentric elements are otherwise identical.
I'm assuming that a Keplerian fit is made to the observed change in angular separation and position angle against time. The shape and orientation of an orbit derived in this way is independent of the barycentre position.
Are you starting from the same place?
Grant
I am not really sure. I tried to minimize assumptions and started right from the equations of motion for two masses m1,m2 in a central potential together with the initial values x(t0), v(t0). The general conic section solution
Code: Select all
x(phi) = p/(1+e*cos(phi))
after splitting off the movement of the barycenter, is obvious.
The less trivial exercise is to use a quite elegant method from my textbook on celestial mechanics to calculate all orbital elements in an arbitrary frame in terms of the initial data for the secondary x(t0), v(t0) in the primary's rest frame. So I have explicit formulae for all orbital parameters and nothing is fitted at that point.
I am still not 100 % sure whether I get entirely the old story...continue working on it...
Bye Fridger
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In my life, being (mostly?) right is a good thing. One snatches what joy one can.t00fri wrote:too bad, you are (mostly?) right, of course.
Okay. I wondered if you were working from (say) proper motions and separations, which would (I think, off the top of my head) produce very different orbits depending on the assumed motion and position of the barycentre.t00fri wrote:I am not really sure.granthutchison wrote:Are we using different assumptions on how these orbits were derived?
I'm assuming that a Keplerian fit is made to the observed change in angular separation and position angle against time. The shape and orientation of an orbit derived in this way is independent of the barycentre position.
Are you starting from the same place?
(Hmmm. Or would the observed separation and proper motions (if measured exactly!) be compatible with only a single barycentre?)
Grant
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Why we need exactly 6 orbital elements to characterize the secondarie's orbit in 3d space?
From what observations are these 6 parameters derived in practice!?
My Solar System Dynamics book isn't here at the mo, but IIRC you need the following to fully describe the orbit in 3D space:
semimajor axis - the distance from the primary.
eccentricity - how non-circular the orbit is.
inclination - angle between a reference plane and the orbital plane.
longitude of pericentre - angle between the pericentre of the orbit and a reference direction.
longitude of ascending node - angle between the reference line in the reference plane and the line where the orbital plane intersects the reference plane (the "line of nodes").
Argument of pericentre - angle within orbital plane between line of nodes and pericentre of orbit.
Also:
The True Anomaly is the angle between the current position of the object in its orbit, and the pericentre of the orbit.
I notice that Celestia uses the Mean Anomaly (M) instead of the True Anomaly. The Mean Anomaly is a rather weird parameter that is pretty damn near impossible to visualise. M is defined as n(T-t) where n is the mean motion, and T-t is the time elapsed since pericentre passage. While it is an angle, it has no simple geometric interpretation.
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Evil Dr Ganymede wrote:Why we need exactly 6 orbital elements to characterize the secondarie's orbit in 3d space?
From what observations are these 6 parameters derived in practice!?
My Solar System Dynamics book isn't here at the mo, but IIRC you need the following to fully describe the orbit in 3D space:
semimajor axis - the distance from the primary.
eccentricity - how non-circular the orbit is.
inclination - angle between a reference plane and the orbital plane.
longitude of pericentre - angle between the pericentre of the orbit and a reference direction.
longitude of ascending node - angle between the reference line in the reference plane and the line where the orbital plane intersects the reference plane (the "line of nodes").
Argument of pericentre - angle within orbital plane between line of nodes and pericentre of orbit.
Also:
The True Anomaly is the angle between the current position of the object in its orbit, and the pericentre of the orbit.
I notice that Celestia uses the Mean Anomaly (M) instead of the True Anomaly. The Mean Anomaly is a rather weird parameter that is pretty damn near impossible to visualise. M is defined as n(T-t) where n is the mean motion, and T-t is the time elapsed since pericentre passage. While it is an angle, it has no simple geometric interpretation.
There is clearly a multitude of different parametrizations one may chose for describing the orbit in space. I am certain that in the approximations I was discussing above there are only 6 independent parameters, corresponding to 3 in x(t0) and 3 in v(t0). If you take nonvanishing m2/m1, there is one more.
Should be obvious? Once you consider the nonvanishing m2/m1 case, you have 7 as I stated above. So your textbook presumably refers to the more general case.
But I think I stated the scenarios clearly above.
Bye Fridger
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Evil Dr Ganymede wrote:Why do you need to worry about reference frames here? Can you not just say the barycentre is fixed in space and everything orbits around it? Isn't that basically the centre of mass of the system?
I think I tried to explain this, too, above. Your statement is only correct in a particular coordinate frame!
In my notation, in frame ii). In the frames i) (observer's rest frame) and iii) (primary's rest frame), the barycenter moves linearly with time. It's the solution of the barycentric equation of motion:
Code: Select all
(m1+m2)* d^2 x_b(t)/dt =0
Since the baricenter moves force free, the rhs is zero!
Upon integration you get the linear movement with time,
x_b(t) = a t + b
with a,b being integration constants. You may chose a special frame with a=b=0. This corresponds to frame ii).
You do not seem to read my posts well before answering. Sorry, if my English makes you suffer...
The statements about the movement of the barycenter are frame dependent. I just can't help that
The physics is, of course independent of the choice of frame, hence we may choose the most convenient one for the problem at hand.
Bye Fridger
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You can get by with either the longitude of the pericentre or the argument of the pericentre, since longitude of pericentre = ascending node + argument of pericentre. The remaining five plus some measure of the anomaly gives you Fridger's six parameters to define an orbit in space.Evil Dr Ganymede wrote:semimajor axis - the distance from the primary.
eccentricity - how non-circular the orbit is.
inclination - angle between a reference plane and the orbital plane.
longitude of pericentre - angle between the pericentre of the orbit and a reference direction.
longitude of ascending node - angle between the reference line in the reference plane and the line where the orbital plane intersects the reference plane (the "line of nodes").
Argument of pericentre - angle within orbital plane between line of nodes and pericentre of orbit.
Also:
The True Anomaly is the angle between the current position of the object in its orbit, and the pericentre of the orbit.
I'm agreeing with Fridger that his seventh parameter (some measure of the mass ratio) does alter the orbital parameters. But I'm sure all it does is allow us to split the original elements into two complementary sets, consisting of two orbits with the same shape and plane as the original, their semimajor axes proportioned according to the mass ratio, and their pericentre arguments opposed - that is, the barycentric orbits of the two components, rather than the body-centred orbit of one component around the other.
Grant
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What is interesting is that the 6th catalog also uses 7 parameters:
Besides the ones that are obvious, and in agreement with what I discussed above,
--semi-major axis (a)
--eccentricity (e)
--inclination (i)
--node (Omega)
--longitude of periastron (w)
--time of periastron passage (T)
they quote as 7th parameter
--the period (P) in years.
Now I wondered what it corresponds to in addition to what I was discussing above.
Clearly the conic section (elliptic orbit) is uniquely specified by the semi-major axis a and the eccentricity e.
The period of the orbit measures according to the 3rd Kepler law for given semi-major axis a, the sum m1+m2 of the masses. Hence, these set the scale for the time-duration of the orbit, but this parameter does not contribute to a specification of it's shape in space.
Any other ideas?
Bye Fridger
Besides the ones that are obvious, and in agreement with what I discussed above,
--semi-major axis (a)
--eccentricity (e)
--inclination (i)
--node (Omega)
--longitude of periastron (w)
--time of periastron passage (T)
they quote as 7th parameter
--the period (P) in years.
Now I wondered what it corresponds to in addition to what I was discussing above.
Clearly the conic section (elliptic orbit) is uniquely specified by the semi-major axis a and the eccentricity e.
The period of the orbit measures according to the 3rd Kepler law for given semi-major axis a, the sum m1+m2 of the masses. Hence, these set the scale for the time-duration of the orbit, but this parameter does not contribute to a specification of it's shape in space.
Any other ideas?
Bye Fridger
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You do not seem to read my posts well before answering. Sorry, if my English makes you suffer...
The english isn't making me suffer, its the maths... (well, maybe it's both. The fact you're not explaining things much in non-mathematical terms probably isn't helping)
Back up a bit though. If you can have a frame of reference where everything in the system orbits the barycentre, why does it have to be moving at all? Wouldn't the barycentre act as if it's an object that has the mass of the two stars, and everything else would follow an elliptical orbit around it?