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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 |
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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!
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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 |
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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. |