ESDU 67004:2004

$62.40

Conversion Formulae for Rotation and Translation of Body Axes

Published By	Publication Date	Number of Pages
ESDU	2004-01	11

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Category: ESDU

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Description

ESDU 67004 relates the vector components, stability derivatives, and inertia parameters in one set of axes to those in another. The axis systems in normal use in flight dynamics are Cartesian body axes with their xz-plane in the plane of symmetry of the aircraft. For this reason ESDU 67004 is restricted to translations of the origin in the xz-plane and rotation about the y-axis.

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