Figure 1 shows the complete three-axis inertial navigation system error diagram. ... The transfer function from gravity deflection to position error is ip = f -g/R(aamp; + C2) s3 + (Cx + C2) s2 + g/R s + C2 g/R ... of the deflection waveform A ac related to the frequency oty as follows: X = vt (v known) or w 2ttv X 2 icy (7) (8) (9) Table 1.

Title | : | Proceedings of First Marine Geodesy Symposium |

Author | : | |

Publisher | : | - 1967 |

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