Euler Angles (Deg) | Rotation Matrix | ||||||||
Yaw | |||||||||
Pitch | |||||||||
Roll | |||||||||
This tool converts Tait-Bryan Euler angles to a rotation matrix, and then rotates the airplane graphic accordingly. The Euler angles are implemented according to the following convention (see the main paper for a detailed explanation):
Gimbal lock occurs when the pitch angle is +90° or -90°. Under these conditions, the yaw and roll axis become aligned and have the same effect.
Comments and error reports may be sent to the following address. We may post comments of general interest. Be sure to identify the page you are commenting on.
.