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Chapter 4: Geometry

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mations of the following types:<br />

1. The identity (which leaves every point fixed)<br />

2. A translation by a vector v<br />

3. A rotation through an angle « around a line Ä<br />

4. A screw motion through an angle « around a line Ä, with displacement <br />

5. A re ection in a plane È<br />

6. A glide-re e ction in a plane È with displacement vector v<br />

7. A rotation-re ection (rotation through an angle « around a line Ä composed<br />

with reflection in a plane perpendicular to Ä).<br />

The identity is a particular case of a translation and of a rotation; rotations are<br />

particular cases of screw motions; reflections are particular cases of glide-reflections.<br />

However, as in the plane case, it is more intuitive to consider each case separately.<br />

4.9.1 FORMULAE FOR SYMMETRIES: CARTESIAN<br />

COORDINATES<br />

In the formulae below, multiplication between a matrix and a triple of coordinates<br />

should be carried out regarding the triple as a column vector (or a matrix with three<br />

rows and one column).<br />

1. Translation by ´Ü ¼ Ý ¼ Þ ¼ µ:<br />

´Ü Ý Þµ ´Ü · Ü ¼ Ý· Ý ¼ Þ· Þ ¼ µ (4.9.1)<br />

2. Rotation through « (counterclockwise) around the line through the origin with<br />

direction cosines (see page 353): ´Ü Ý Þµ Å ´Ü Ý Þµ where Å is<br />

¾the matrix<br />

¿<br />

¾´½ Ó× «µ ·Ó׫ ´½ Ó× «µ ×Ò « ´½ Ó× «µ · ×Ò «<br />

´½ Ó× «µ · ×Ò « ¾´½ Ó× «µ · Ó× « ´½ Ó× «µ ×Ò « <br />

´½ Ó× «µ ×Ò « ´½ Ó× «µ · ×Ò « ¾´½ Ó× «µ · Ó× «<br />

(4.9.2)<br />

3. Rotation through « (counterclockwise) around the line with direction cosines<br />

through an arbitrary point ´Ü ¼ Ý ¼ Þ ¼ µ:<br />

´Ü Ý Þµ ´Ü ¼ Ý ¼ Þ ¼ µ·Å ´Ü Ü ¼ Ý Ý ¼ Þ Þ ¼ µ (4.9.3)<br />

where Å is given by Equation (4.9.2).<br />

4. Arbitrary rotations and Euler angles: Any rotation of space fixing the origin<br />

can be decomposed as a rotation by about the Þ-axis, followed by a rotation<br />

by about the Ý-axis, followed by a rotation by about the Þ-axis. The<br />

numbers , , and are called the Euler angles of the composite rotation,<br />

which acts as: ´Ü Ý Þµ Å ´Ü Ý Þµ where Å is the matrix given by<br />

¾<br />

<br />

Ó× Ó× Ó× ×Ò ×Ò ×Ò Ó× Ó× Ó× ×Ò ×Ò Ó× <br />

Ó× Ó× ×Ò ·×Ò Ó× ×Ò Ó× ×Ò · Ó× Ó× ×Ò ×Ò <br />

Ó× ×Ò ×Ò ×Ò Ó× <br />

(4.9.4)<br />

¿<br />

© 2003 by CRC Press LLC

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