"Single particle dynamics" is perhaps
the most important introductory aspect of plasma theory, especially
for space plasmas (e.g. Earth's magnetosphere, heliosphere etc.). Specifically,
it is the domain wherein we enter plasma “orbit theory” and consider a charged
particle (say of charge q) in a uniform and constant magnetic field (B).
The behavior of such charges, in both magnetic and electric fields, is crucial
for understanding plasma behavior as a whole.
The governing equation of motion with F the Lorentz force, is:
m (dv/dt) = q(v X B) = F
The motion here is such that v will always be perpendicular to the force acting on the particle so v ⊥ F, implying circular motion. Thus:
dv/dt = q/ m [v X B]
Meanwhile, (v⊥ ) 2 / r = q/ m [v⊥ B]
The quantity r above is none other than the gyro-radius. Solving for it one finds:
r = m/ q [v⊥ / B] = v⊥ / (qB/m) = v⊥ / Ω
for which one can have either the electron, or ion gyro-frequency (Ω). The ion gyrofrequency will be:
Ω i = qB/ m i
And the electron gyrofrequency is:
Ω e = qB/ m e
These equations help to explain the physical basis for the origin of a preponderance of radio waves (i.e. gyro-magnetic emission) such as from the Sun, and other cosmic objects (e.g. quasars, pulsars).
Note that the velocity v has two components, parallel and perpendicular:
v = v|| + v⊥
where the first term denotes the velocity along B which stays constant so that d(v|| )/ dt = 0.
Further, we have:
v⊥2/ r = q/ m [v⊥ · B](setting the centripetal force = to the magnetic force producing it)
From the preceding we obtain the gyro frequencies.
While on this topic it is useful to also consider the "gyration velocity" which is simply the magnitude:
v⊥ = 2 m m B/ m
where m m is the magnetic moment.
Thus, the proton gyrates at this rate provided m m is a constant of the motion: viz. m m = m(v⊥)2/ 2B = const .
The gyro-period is: T = 2 p / Ω
Bear in mind the gyration energy:
E = m m B = m/2 (E/B) 2,
Note that the position of a particle at any time t can always be specified for a given coordinate system, if one knows the Larmor radius r and the gyrofrequency, Ω:
Thus: r(t)= r (cos Ω t x^ - sin Ω t y^)
Which equation can be referenced to the diagram below:
The basics presented above ignore the fact that no general
solution exists to the equations of motion for a charged particle moving under
the influence of the Lorentz force in a dipole B-field.
What happens is that an approximation is needed, called “the guiding center
(GC) approximation”. This assumes the magnetic field changes are
small over a gyroperiod, and gyroradius.
If a charged particle is moving through a converging magnetic field, i.e. a magnetic 'bottle such as shown below:
Then it gyrates in increasingly tighter circles, but the speed of its circular motion increases. The kinetic energy involved in this circular motion also increases but the total kinetic energy remains constant, so the kinetic energy of this circular motion comes at the expense of the particle's forward motion along field lines. The farther the charged particle moves toward one end of a magnetic bottle, the slower it goes in that direction.
Based on this simplification, the electron or ion moves along
B-field referenced to a guiding center, such that:
(a ) x – xo = - i v⊥ exp (i Ω t)/ W = r sin (Ω t)
and
(b) y – yo = ± v⊥ exp (i Ω t)/ W = r cos (Ω t)
The key point is that the guiding center (xo, yo)
is fixed. while r is the "Larmor radius" (or gyroradius).
In the GC approximation, particle motion displays three components:
1) gyration about a field line (given by the gyrofrequency, or
cyclotron frequency);
2) reflection between two mirror points (embodied by the
“bounce period”) and
3) a gradual longitudinal drift, denoted by the (E x
B) drift.
Suggested Problems:
1)Given the situation shown below for a particle in plasma:
And: v o = v xo x^
+ v yo y^ (for initial velocity)
Solve the equation of motion: F = q(E + v
X B)
2) (a)If the perpendicular velocity component ( v⊥) is 105 m/s for
an electron in a plasma, find its Larmor radius, gyration energy and its
gyro-period.
(b) Find the guiding center positions for the electron
referenced in (a) if t = T/2.


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