Chatroom
 

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Bad Astronomy and Universe Today Forum > Space and Astronomy > Astronomy
Register FAQ Members List Calendar Mark Forums Read

   

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
  #61 (permalink)  
Old 29-May-2006, 08:59 PM
grant hutchison grant hutchison is offline
Senior Member
 
Join Date: Jul 2005
Posts: 5,512
Default

And, just out of interest, the trajectory of an object falling off the inner colinear Lagrangian:

L1escape.jpg

It ends up confined to the inner slope of the potential surface, rather than moving locally around the Lagrangian point. In the non-rotating frame, of course, it's in an elliptical orbit with a period considerable shorter than the co-rotating frame. But it's doomed to have a close encounter with the secondary mass at some time in the future.

Grant Hutchison

Last edited by grant hutchison; 04-June-2006 at 09:03 PM. Reason: Revised URL link
Reply With Quote
  #62 (permalink)  
Old 30-May-2006, 03:04 AM
hhEb09'1's Avatar
hhEb09'1 hhEb09'1 is offline
Senior Member
 
Join Date: Apr 2005
Location: NC USA
Posts: 8,224
Default

Quote:
Originally Posted by Ken G
the result is always informative in one way or another!)
d*rn straight!
Quote:
You're right, you can make that work by starting the object stuck to the record, and then letting it go so that it's frictionless. That would be easier than using a magnetic field, and might actually make a darn interesting demonstration for an advanced orbital mechanics course!
I'm in. I suppose the first step is to calculate something...
Reply With Quote
  #63 (permalink)  
Old 30-May-2006, 08:35 AM
Ken G's Avatar
Ken G Ken G is offline
Senior Member
 
Join Date: Oct 2005
Posts: 10,541
Default

Quote:
Originally Posted by grant hutchison
You can see this one having a dangerously close approach to the Jupiter-mass after overtaking the trailing Trojan point and before turning back to complete the horseshoe orbit. (When I was watching the simulation drawing this one, I thought it wasn't going to turn around.)
You can really see the instability/stability/instability aspects of this complex system from your pictures. It's obviously hard to make too many sweeping generalizations about what will happen. I also note that for L1, it only takes one orbit to get to the other side of the system (assuming each swoop is an orbit), whereas for the horseshoe orbits around L4, it takes about 10. Nevertheless, that's only an order of magnitude difference. Maybe it takes a pretty big perturbation to get into the horseshoe mode? A pretty neat simulation. You really ought to be able to buy rotating surfaces bent to the shape of that effective potential, and be able to launch beads or whatever to see these kinds of orbits in a demonstration or a tabletop toy.
Reply With Quote
  #64 (permalink)  
Old 30-May-2006, 11:12 AM
grant hutchison grant hutchison is offline
Senior Member
 
Join Date: Jul 2005
Posts: 5,512
Default

Quote:
Originally Posted by Ken G
You really ought to be able to buy rotating surfaces bent to the shape of that effective potential, and be able to launch beads or whatever to see these kinds of orbits in a demonstration or a tabletop toy.
You wouldn't want to use an effective potential map, as in Cornish's article, though; just a model of the gravitational potential of the two objects. Otherwise you have centrifugal force both embedded in the model and arising from the model's rotation.

Grant Hutchison
Reply With Quote
  #65 (permalink)  
Old 30-May-2006, 11:37 AM
grant hutchison grant hutchison is offline
Senior Member
 
Join Date: Jul 2005
Posts: 5,512
Default

Quote:
Originally Posted by grant hutchison
You wouldn't want to use an effective potential map, as in Cornish's article, though; just a model of the gravitational potential of the two objects. Otherwise you have centrifugal force both embedded in the model and arising from the model's rotation.
In fact, won't you need to distort your model gravity field in order to ameliorate the centrifugal force arising from its own rotation? Centrifugal force increases with the square of omega, whereas Coriolis force varies directly. (I'm assuming the reduction in modelled r will be offset by the reduction in modelled v.) If your model is to turn in less than the period of revolution of the modelled system (which is presumably desirable), it's going to need an "anticentrifugal" bias built in, isn't it?

Grant Hutchison
Reply With Quote
  #66 (permalink)  
Old 30-May-2006, 11:39 AM
hhEb09'1's Avatar
hhEb09'1 hhEb09'1 is offline
Senior Member
 
Join Date: Apr 2005
Location: NC USA
Posts: 8,224
Default

Oops. The hills have disappeared.
Reply With Quote
  #67 (permalink)  
Old 30-May-2006, 01:49 PM
Ken G's Avatar
Ken G Ken G is offline
Senior Member
 
Join Date: Oct 2005
Posts: 10,541
Default

Quote:
Originally Posted by grant hutchison
You wouldn't want to use an effective potential map, as in Cornish's article, though; just a model of the gravitational potential of the two objects.
Oops, you're right, I was still thinking in terms of the magnetic field.
Reply With Quote
  #68 (permalink)  
Old 30-May-2006, 01:54 PM
Ken G's Avatar
Ken G Ken G is offline
Senior Member
 
Join Date: Oct 2005
Posts: 10,541
Default

Quote:
Originally Posted by grant hutchison
If your model is to turn in less than the period of revolution of the modelled system (which is presumably desirable), it's going to need an "anticentrifugal" bias built in, isn't it?
That might be a clever way to go, but I think more straightforward would be to simply tune omega to the "orbital period", as it were. Of course that wouldn't be Jupiter's orbital period, but you can tune it by altering the steepness of the potential hills. Choose the omega, then set the steepness to keep the bead in equilibrium at L4. But this is even better than an effective potential, as people can better picture the real potential I should think.
Reply With Quote
  #69 (permalink)  
Old 30-May-2006, 02:16 PM
Ken G's Avatar
Ken G Ken G is offline
Senior Member
 
Join Date: Oct 2005
Posts: 10,541
Default

In fact, how cool would an amusement park ride based on this principle be? You'd have a very steep and slippery potential hill, and spin it up, and let people walk or slide around somehow. They'd find, despite their intuition about the shape of the hills, that they followed your orbits!
Reply With Quote
  #70 (permalink)  
Old 30-May-2006, 05:53 PM
grant hutchison grant hutchison is offline
Senior Member
 
Join Date: Jul 2005
Posts: 5,512
Default

Quote:
Originally Posted by Ken G
That might be a clever way to go, but I think more straightforward would be to simply tune omega to the "orbital period", as it were.
No, my worry was that coriolis and centrifugal seemed to follow different scaling laws in their relationship with omega, so the behaviour of a slow rotator wouldn't be reproduced by a fast rotator.
This didn't seem to make sense, however, since the stability considerations for the Trojan vicinity involve only the mass ratio and the assumption of circular orbits.
As an example, say we modelled the Jupiter-Sun Trojans by reducing the linear dimensions by a factor of 1011 and increasing the angular velocity by a factor of 107. This would produce something 16m across rotating once in 37s, so it would fit with your fairground ride.
Centrifugal force would scale with ωČr, so would increase by a factor of 103. This could be compensated by reducing the modelled masses by a factor of 1019, so that gravity, scaling with M/rČ, would also increase by a factor of 103.
So far so good. But Coriolis, scaling with ωv, looked like it should scale as 107x10-11 = 10-4. Yikes. Didn't make sense, from the stability criteria.
What I was missing is that the velocity needs to scale not just with the change in linear dimensions, but also with the change in the characteristic time for the system. That gives me another factor of 107 for the Coriolis force, and it settles into line with the other forces, with a thousand-fold increase.

Grant Hutchison
Reply With Quote
  #71 (permalink)  
Old 30-May-2006, 07:04 PM
hhEb09'1's Avatar
hhEb09'1 hhEb09'1 is offline
Senior Member
 
Join Date: Apr 2005
Location: NC USA
Posts: 8,224
Default

Quote:
Originally Posted by Ken G
But this is even better than an effective potential, as people can better picture the real potential I should think.
Let's make it on the order of a meter in radius--we can sell it to every math/science/exploritorium in the country.
Reply With Quote
  #72 (permalink)  
Old 30-May-2006, 08:48 PM
DyerWolf DyerWolf is offline
Senior Member
 
Join Date: May 2006
Location: The Dark Side of the Sun
Posts: 1,015
Default

Found this simulator which looks interesting. (Takes a while to load sometimes). I found it interesting to watch the L1,2 and 3 satellites' paths once they were perturbed from their initial positions.

http://www.princeton.edu/~rvdb/JAVA/...y/Galaxy1.html

Load the L1-L5 M/m=40 simulation and let it run until L3 starts wandering.
Reply With Quote
  #73 (permalink)  
Old 02-June-2006, 03:20 PM
Ken G's Avatar
Ken G Ken G is offline
Senior Member
 
Join Date: Oct 2005
Posts: 10,541
Default

Yeah, that's cute, and yeah, there's a lot of money to made on the rotating plastic sheet!
Reply With Quote
  #74 (permalink)  
Old 29-June-2006, 09:36 PM
publiusr publiusr is offline
Senior Member
 
Join Date: Feb 2005
Posts: 4,292
Default

Nice links!
Reply With Quote
Reply


Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are On
Pingbacks are On
Refbacks are On



All times are GMT. The time now is 06:00 AM.


Powered by vBulletin® Version 3.7.3
Copyright ©2000 - 2008, Jelsoft Enterprises Ltd.
LinkBacks Enabled by vBSEO 3.0.0
©  2006 Bad Astronomy and Universe Today