Figure 1 shows the complete three-axis inertial navigation system error diagram. ... The transfer function from gravity deflection to position error is Aaamp; = a f Al3 -g/R (aamp; + C2) + (Cx + C2) s2 + g/R s + C2 g/R (2) The gains ... frequency (t\p as follows : \ = vt (v known) co alt;p t or Ualt;P = X = 2vv X 2 irv (7) (8) (9) 1/5 1/R 6p FIGURE 2.

Title | : | Proceedings of ... Marine Geodesy Symposium |

Author | : | |

Publisher | : | - 1967 |

Continue