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Fig. 5 Tadpoles-Horseshoes

 

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Summary
Intro and History
Newton’s Gravity
Trojan Points and Bodies
Tadpole-Horseshoe Orbits
... Oversights
21st Century Astronomy
APPENDIX
Fig. 1 Bodies and Vectors
Fig. 2 Falling Rate Diff.
Fig. 3 Centers of Mass
Fig. 4 Lagrangian Points
Fig. 5 Tadpoles-Horseshoes
Fig. 6a Ternaries?
Fig. 6b Ternaries?
Author

Newton’s... Oversight
Einstein’s... Oversights
Entropy’s... Oversights
Comet Origins
Cosmology... Oversights
Creationism... Oversights

Newton’s Great... Oversight
Galileo’s Falling Bodies and Lagrange’s Trojan Asteroids
With Their Tadpole and Horseshoe Orbits

 

8          FIGURES (cont.)

tadpole and horshoe orbits

Temporary explanation of what's what (compare to Figure 4): on the central vertical line: L4 and L5 lie on either side of the central horizontal line, just past the first horizontal line in either direction away from the central line; on the central horizontal line: L3 lies between the second and third vertical lines left of the central vertical line; m1(largest mass) lies just inside the first vertical line left of the central line; L1 lies between the central vertical line and the first vertical line right of the central line;  m2 (second largest mass) lies just inside the first vertical line right of the central line;  L2 lies just outside the first vertical line to the right of the central line.

Figure 5. “Tadpole” and “horseshoe” orbits.

This contour plot gives some idea of what “tadpole” and “horseshoe” orbits are about. It plots a function of the falling rate difference that indicates the rate at which a (static) triangle of masses, with the “infinitesimal” body at L4 (or L5) perturbed (to the point on the plot), further degrades from equilateral. The degradation is least quick in the tadpoles, quicker in the horseshoes, to very much quicker outside them. The largest mass is set to “1”; the second largest mass is 0.01 m1, i.e. smaller than the ~0.04 m1 that Lagrange’s analysis indicated was the upper level for m2 that allowed stability (reminder: with the 3rd mass “infinitesimal”); the smallest mass is 0.0001 m1, and so approximates “infinitesimal”.

The “centers” of the mirror-symmetric tadpoles — L4 and L5 — lie on the vertical x = 0 line, roughly 0.866 above and below the y = 0 line.

L1, L2 and L3 all lie on the horizontal y = 0 line. On this plot, L1 is about x = 0.3, L2 about x = 0.9, and L3 about x = -1.5.Regarding L3, the more equal the 2 smaller masses are, the more likely that they — one of them at L3 — will be the same distance from the largest mass.

NOTE how the tadpoles “grow” till they meet and form an oddly shaped horseshoe, one which covers L3. L3 is actually in a place where the (degenerate) triangle degrades roughly as fast as it does in the tadpoles. This suggests that L3 should be thought of as stable if the horseshoe orbits are considered stable!... unless e.g. the velocity through L3 is critical to its returning, and could not generally be obtained by “wandering away, perturbed” from L3.

NOTE ALSO: a contour plot is like a topographical map: the shape of the contour lines depends on the “elevation” of the intersections of various “cutting planes” with the function’s 3-dimensional surface. The contour lines of the same surface can look quite different if contour-plotted slightly differently.

NOTE: we think of the asteroid as being in a tadpole or horseshoe orbit with regard to e.g. the Earth or Jupiter, since we are looking at its orbit from an Earth or Jupiter relative reference frame. If we look at the orbit from a frame that is where Earth would be if there were no asteroid, and look at both the Earth and the asteroid orbiting, the Earth will also be seen to have its own “tadpole” or “horseshoe” type movement, but smaller as its mass is larger. The asteroid’s orbit will also have a somewhat different shape. If the masses are more equal, the orbits can take on very different shapes. See examples of possible shapes in Figure 6b, which has all 3 masses equal.

ALSO NOTE: technically, the Lagrangian points would not even exist if Lagrange’s restriction on relative mass, i.e. that m< ~0.04 m1, is not met.

FURTHER, NOTE that this 2 dimensional plot is inadequate to give a picture of e.g. the dynamics of the Earth companion asteroid, 3753 Cruithne, with its highly inclined orbit that takes it directly above Earth.

(Plotted with Mathcad 2000.)

 

 

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