IHS ESDU Conversion formulae for rotation and translation of body axes. 67004

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.
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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Conversion formulae for rotation and translation of body axes. - 67004 - IHS ESDU
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Conversion formulae for rotation and translation of body axes.
67004
Conversion formulae for rotation and translation of body axes. 67004
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.

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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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 67004
Product Name Conversion formulae for rotation and translation of body axes.
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