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DICTIONARY OF GEOPHYSICS, ASTROPHYSICS, and ASTRONOMY

DICTIONARY OF GEOPHYSICS, ASTROPHYSICS, and ASTRONOMY

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L<br />

lagoon A shallow, sheltered bay that lies between<br />

a reef <strong>and</strong> an isl<strong>and</strong>, or between a barrier<br />

isl<strong>and</strong> <strong>and</strong> the mainl<strong>and</strong>.<br />

Lagrange points Five locations within a<br />

three-body system where a small object will always<br />

maintain a fixed orientation with respect to<br />

the two larger masses though the entire system<br />

rotates about the center of mass. If the largest<br />

mass in the system is indicated by M1 <strong>and</strong> the<br />

second largest mass is M2, the five Lagrange<br />

points are as follows: in a straight line with M1<br />

<strong>and</strong> M2 <strong>and</strong> just outside the orbit of M2 (usually<br />

called the L1 point); in a straight line with M1<br />

<strong>and</strong> M2 <strong>and</strong> just inside the orbit of M2 (L2); in<br />

a straight line with M1 <strong>and</strong> M2 <strong>and</strong> located in<br />

M2’s orbit 180 ◦ away from M2 (i.e., on the other<br />

side of M1) (L3); <strong>and</strong> 60 ◦ ahead <strong>and</strong> behind M2<br />

within M2’s orbit (L4 <strong>and</strong> L5). In the sun-Jupiter<br />

system, the Trojan asteroids are found at the L4<br />

<strong>and</strong> L5 locations. In the Earth-sun system, the<br />

Lagrangian points L1 <strong>and</strong> L2 are both on the sun-<br />

Earth line, about 236 RE (≈ 0.01 AU) sunward<br />

<strong>and</strong> anti-sunward of Earth, respectively. The<br />

other points are far from Earth <strong>and</strong> therefore too<br />

much affected by other planets to be of much<br />

use, e.g., L3 on the Earth-sun line but on the far<br />

side of the sun. However, L1 (or its vicinity) is a<br />

prime choice for observing the solar wind before<br />

it reaches Earth, <strong>and</strong> L2 is similarly useful for<br />

studying the distant tail of the magnetosphere.<br />

Spacecraft have visited both regions — ISEE-3,<br />

WIND, SOHO <strong>and</strong> ACE that of L1, ISEE-3 <strong>and</strong><br />

GEOTAIL that of L2. Neither equilibrium is<br />

stable, <strong>and</strong> for this <strong>and</strong> other reasons spacecraft<br />

using those locations require on-board propulsion.<br />

Of the Lagrangian points of the Earth-moon<br />

system, the two points L4 <strong>and</strong> L5, on the moon’s<br />

orbit but 60 ◦ on either side of the moon, have<br />

received some attention as possible sites of space<br />

colonies in the far future. Their equilibria are<br />

stable.<br />

© 2001 by CRC Press LLC<br />

Lagrangian<br />

Lagrangian In particle mechanics, a function<br />

L = L(x i ,dx j /dt, t) of the coordinate(s)<br />

of the particle x i , the associated velocity(ies)<br />

dx j /dt, <strong>and</strong> the parameter t, typically time,<br />

such that the equations of motion can be written:<br />

d<br />

dt<br />

∂<br />

∂L<br />

∂x i<br />

∂t<br />

− ∂L<br />

= 0 .<br />

∂xi In this equation (Lagrange’s equation) the partial<br />

derivatives are taken as if the coordinates<br />

xi <strong>and</strong> the velocities dxj /dt were independent.<br />

The explicit d/dt acting on ∂L<br />

∂( ∂xi differentiates<br />

∂t )<br />

xi <strong>and</strong> dxi /dt. For a simple Lagrangian with<br />

conservative potential V ,<br />

L = T − V = 1<br />

2 m <br />

dx i 2 <br />

j<br />

/dt − V x ,<br />

one obtains the usual Newtonian equation<br />

d<br />

dt mdxi<br />

dt =−∂V .<br />

∂xi Importantly, if the kinetic energy term T <strong>and</strong><br />

the potential V in the Lagrangian are rewritten<br />

in terms of new coordinates (e.g., spherical), the<br />

equations applied to this new form are again the<br />

correct equations, expressed in the new coordinate<br />

system.<br />

A Lagrangian of the form L = L(xi ,dxj /dt,<br />

t) will produce a resulting equation that is second<br />

order in time, as in Newton’s equations. If<br />

the Lagrangian contains higher derivatives of the<br />

coordinates, then Lagrange’s equation must be<br />

modified. For instance, if L contains the acceleration,<br />

a j = d2x j<br />

,<br />

dt2 so that<br />

L = L<br />

<br />

x i ,dx j /dt, d 2 x k /dt 2 <br />

,t ,<br />

the equation of motion becomes<br />

− d2<br />

dt 2<br />

∂<br />

∂L<br />

d 2 x i<br />

dt 2<br />

+ d<br />

dt<br />

∂<br />

∂L<br />

∂x i<br />

∂t<br />

− ∂L<br />

= 0 ,<br />

∂xi which will in general produce an equation of motion<br />

containing third time derivatives. The presence<br />

of higher derivatives in the Lagrangian produces<br />

higher order derivatives in the equation of

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