Difference between revisions of "Sadiq Proposal Defense"

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For the convenience of representation, we use <math>z</math> to represent our transverse coordinates, while discussing emittance. And we would like to express longitudinal beam direction with <math>s</math>. Our transverse beam profile changes along the beam line, it makes <math>z</math> is function of <math>s</math>, <math>z~(s)</math>. The angle of a accelerated charge regarding the designed orbit can be defined as:
 
For the convenience of representation, we use <math>z</math> to represent our transverse coordinates, while discussing emittance. And we would like to express longitudinal beam direction with <math>s</math>. Our transverse beam profile changes along the beam line, it makes <math>z</math> is function of <math>s</math>, <math>z~(s)</math>. The angle of a accelerated charge regarding the designed orbit can be defined as:
<math>z'=frac{dz}{ds}</math>
+
<math>z'=\frac{dz}{ds}</math>
  
  

Revision as of 18:49, 20 August 2011

Emittance

What is Emittance

In accelerator physics, Cartesian coordinate system was used to describe motion of the accelerated particles. Usually the z-axis of Cartesian coordinate system is set to be along the electron beam line as longitudinal beam direction. X-axis is set to be horizontal and perpendicular to the longitudinal direction, as one of the transverse beam direction. Y-axis is set to be vertical and perpendicular to the longitudinal direction, as another transverse beam direction.

For the convenience of representation, we use [math]z[/math] to represent our transverse coordinates, while discussing emittance. And we would like to express longitudinal beam direction with [math]s[/math]. Our transverse beam profile changes along the beam line, it makes [math]z[/math] is function of [math]s[/math], [math]z~(s)[/math]. The angle of a accelerated charge regarding the designed orbit can be defined as: [math]z'=\frac{dz}{ds}[/math]


File:Emittance.tex


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