Chapter 4: Geometry
Chapter 4: Geometry
Chapter 4: Geometry
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
esults hold at point f´Øµ of :<br />
x¼¼ ¢ x ¼ <br />
x ¼ <br />
¿ x¼ ¡ ´x ¼¼ ¢ x ¼¼¼ µ<br />
x ¼ ¢ x ¼¼ (4.20.3)<br />
¾<br />
The vectors of the moving trihedron satisfy the Serret–Frenet equations<br />
t n n t · b b n (4.20.4)<br />
For any plane curve represented parametrically by x f´Øµ ´Ø ´Øµ ¼µ,<br />
<br />
<br />
¬<br />
¬ ¾ Ü ¬¬<br />
Ø ¾ ¡ ¾<br />
¿¾<br />
(4.20.5)<br />
½· Ü<br />
Ø<br />
Expressions for the curvature vector and curvature of a plane curve corresponding to<br />
different representations are given in the following table:<br />
Representation Curvature vector k Curvature, ½<br />
Ü ´Øµ<br />
Ý ´Øµ<br />
Ý ´Üµ<br />
Ö ´µ<br />
´ÜĐÝ ÝĐܵ<br />
´Ü ¾ · Ý ¾ µ ¾ ´ Ý ÜĐÝ ÝĐÜ<br />
ܵ<br />
´Ü ¾ · Ý ¾ µ ¿¾<br />
Ý ¼¼<br />
Ý ¼¼ <br />
´½ · Ý ¼¾ µ ´ ݼ ½µ<br />
¾ ´½ · Ý ¼¾ µ ¿¾<br />
´Ö ¾ ·¾Ö ¼ ¾<br />
ÖÖ ¼¼ µ ´ Ö ×Ò Ö Ó× Ö ¾ ·¾Ö ¼ ¾<br />
ÖÖ ¼¼<br />
´Ö ¾ · Ö ¼ ¾ µ<br />
¾ Ö Ó× Ö ×Ò µ ´Ö ¾ · Ö ¼ ¾ µ<br />
¿¾<br />
The equation of the osculating circle of a plane curve is given by<br />
where c x · ¾ k is the center of curvature.<br />
´y cµ ¡ ´y cµ ¾ (4.20.6)<br />
THEOREM 4.20.1<br />
(Fundamental existence and uniqueness theorem)<br />
Let ´×µ and ´×µ be any continuous functions de ne d for all × ¾ ℄. Then there<br />
exists, up to a congruence, a unique space curve for which is the curvature<br />
function, is the torsion function, and × an arc length parameter along .<br />
4.20.1.3 Example<br />
A regular parametric representation of the circular helix is given by x f´Øµ <br />
´ Ó× Ø ×Ò Ø Øµ, for all Ø ¾ Ê, where ¼ and ¼are constant. By successive<br />
differentiation,<br />
x ¼ ´ ×Ò Ø Ó× Ø µ<br />
x ¼¼ ´ Ó× Ø ×Ò Ø ¼µ<br />
x ¼¼¼ ´<br />
so that ×<br />
Ø x¼ <br />
Ô<br />
¾ · ¾ . Hence,<br />
×Ò Ø Ó× Ø ¼µ<br />
1. Arc length parameter: × «´Øµ Ø´ ¾ · ¾ µ ¾<br />
½<br />
2. Curvature vector: k t<br />
× Ø t<br />
× Ø ´¾ · ¾ µ ½´ Ó× Ø ×Ò Ø ¼µ<br />
(4.20.7)<br />
© 2003 by CRC Press LLC