To express the change in the moment of momentum in detail, the concept of a differential rotation is needed. In the plane, it is straightforward to define ; however, for , it is more complicated. One choice is to define derivatives with respect to yaw-pitch-roll variables, but this leads to distortions and singularities, which are problematic for the Newton-Euler formulation. Instead, a differential rotation is defined as shown in Figure 13.11. Let denote a unit vector in , and let denote a rotation that is analogous to the 2D case. Let denote the angular velocity vector,

(13.83) |

This provides a natural expression for angular velocity.

This relationship can be used to derive expressions that relate to yaw-pitch-roll angles or quaternions. For example, using the yaw-pitch-roll matrix (3.42) the conversion from to the change yaw, pitch, and roll angles is

Steven M LaValle 2012-04-20