COMPLEX NAVIGATION SYSTEM
FIELD: aircraft engineering. ^ SUBSTANCE: system additionally has analysis block, first, second and third inputs/outputs of which are connected to second input/output of prediction block, second input/output of filter selection block, input/output of block for selecting correcting means respectively...
Saved in:
Main Authors | , , , , , , , , , , , |
---|---|
Format | Patent |
Language | English Russian |
Published |
27.11.2005
|
Edition | 7 |
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | FIELD: aircraft engineering. ^ SUBSTANCE: system additionally has analysis block, first, second and third inputs/outputs of which are connected to second input/output of prediction block, second input/output of filter selection block, input/output of block for selecting correcting means respectively. One-direction input of analysis block is connected to output of block for generating status parameters and to second input of block for compensating for errors. Block for selecting correcting means is connected to appropriate outputs of block of correcting means. One-direction output of block for selecting correcting means is connected to second input of block for forming discrepancy, and input/output of block for selecting correcting means is connected to third input/output of analysis block. ^ EFFECT: broader functional capabilities. ^ 1 dwg |
---|---|
Bibliography: | Application Number: RU20040108184 |