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3.4.5 Attitude Models

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Attitude models for inertial navigation represent


Figure 3.12 Radii of WGS84 reference ellipsoid.

1 The relative rotational orientations of two coordinate systems, usually represented by coordinate transformation matrices but also represented in terms of rotation vectors.

2 Attitude dynamics, usually represented in terms of three‐dimensional rotation rate vectors but also represented by four‐dimensional quaternion.

Global Navigation Satellite Systems, Inertial Navigation, and Integration

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