The horizontal components of (1) can then be written as SRU alt;tagt;v = in -r aamp;RX a ( 9) (10) The time derivatives of (9) and (10) ... Consequently, the position error equations valid for an hour or so of navigation time will simply be presented. ... ( 13) and (14) may be presented in block diagram form, as shown in Fig. ... Cxg Cw Czy lr 1.. -Cxt Cy, Cz.l Liz Cx, jT ^V.xT Lz, xT aquot;1. ^aix.yT i-a#39;ViVT Cz, yT 1. -Cx, zT ^ai U, zT.

Title | : | IEEE Transactions on Aerospace and Navigational Electronics |

Author | : | |

Publisher | : | - 1961 |

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