Attitude: Difference between revisions
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| style="padding: 12px;" | $$\operatorname{att}(\mathbf g) = g_x \mathbf e_{23} + g_y \mathbf e_{31} + g_z \mathbf e_{12}$$ | | style="padding: 12px;" | $$\operatorname{att}(\mathbf g) = g_x \mathbf e_{23} + g_y \mathbf e_{31} + g_z \mathbf e_{12}$$ | ||
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== In the Book == | |||
* The attitude is discussed in Section 2.8.4. |
Latest revision as of 05:13, 13 April 2024
The attitude function, denoted by $$\operatorname{att}$$, extracts the attitude of a geometry and returns a purely directional object. The attitude function is defined as
- $$\operatorname{att}(\mathbf u) = \mathbf u \vee \overline{\mathbf e_4}$$ .
The attitude of a line is the line's direction as a vector, and the attitude of a plane is the plane's normal as a bivector.
The following table lists the attitude for the main types in the 4D rigid geometric algebra $$\mathcal G_{3,0,1}$$.
Type | Definition | Attitude |
---|---|---|
Magnitude | $$\mathbf z = x \mathbf 1 + y {\large\unicode{x1d7d9}}$$ | $$\operatorname{att}(\mathbf z) = y \mathbf e_{321}$$ |
Point | $$\mathbf p = p_x \mathbf e_1 + p_y \mathbf e_2 + p_z \mathbf e_3 + p_w \mathbf e_4$$ | $$\operatorname{att}(\mathbf p) = p_w \mathbf 1$$ |
Line | $$\boldsymbol l = l_{vx} \mathbf e_{41} + l_{vy} \mathbf e_{42} + l_{vz} \mathbf e_{43} + l_{mx} \mathbf e_{23} + l_{my} \mathbf e_{31} + l_{mz} \mathbf e_{12}$$ | $$\operatorname{att}(\boldsymbol l) = l_{vx} \mathbf e_1 + l_{vy} \mathbf e_2 + l_{vz} \mathbf e_3$$ |
Plane | $$\mathbf g = g_x \mathbf e_{423} + g_y \mathbf e_{431} + g_z \mathbf e_{412} + g_w \mathbf e_{321}$$ | $$\operatorname{att}(\mathbf g) = g_x \mathbf e_{23} + g_y \mathbf e_{31} + g_z \mathbf e_{12}$$ |
In the Book
- The attitude is discussed in Section 2.8.4.