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Kinematics and dynamics of rigid bodies 31<br />

Note that the convention used here in Figure 2.10 is based on a set of Body<br />

(X-Y-Z) rotations. It will be shown later that different conventions may be<br />

used such as the Yaw-Pitch-Roll method based on a set of Body (Z-Y-X)<br />

rotations or the Euler angle method used in MSC.ADAMS that is based on<br />

a Body (Z-X-Z) combination.<br />

2.2.7 Vector transformation<br />

In multibody systems analysis it is often necessary to transform the components<br />

of a vector measured parallel to the axis of one reference frame to<br />

those measured parallel to a second reference frame. These operations<br />

should not be confused with vector rotation. In a transformation it is the<br />

magnitude and direction of the components that change. The direction of<br />

the vector is unchanged. Consider the transformation of a vector {A} 1, or in<br />

full definition {A} 1/1 , from reference frame O 1 to reference frame O 2 .<br />

Figure 2.11 represents a view back along the X 1 -axis towards the origin O 1 .<br />

The reference frame O 2 is rotated through an angle about the X 1 -axis of<br />

frame O 1 .<br />

From Figure 2.11 it can be seen that<br />

Ax2 Ax1<br />

Ay2 Ay1 cos Az1<br />

sin <br />

Az Ay sin<br />

cos<br />

2 1 1<br />

(2.27)<br />

Z 1<br />

Az 1 sin α<br />

Ay 2<br />

Ay 1 cos α<br />

Ay 1 sin α<br />

α<br />

A<br />

{A} 1/2<br />

Az 2<br />

Az 1 cos α<br />

Z 2<br />

Ay 1<br />

Az 1<br />

Az 1 sin α<br />

{A} 1/1<br />

Y 1<br />

α<br />

Ay 1 sin α<br />

Y 2<br />

α<br />

O 1<br />

O 2<br />

Fig. 2.11<br />

Transformation of a vector

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