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...

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Main Authors DZHANDZHGAVA G.I, SHKRED V.K, KAVINSKIJ V.V, BABICHENKO A.V, OREKHOV M.I, ROGALEV A.P, BRAZHNIK V.M, NIKULIN A.S, SHELEPEN' K.V, SUKHORUKOV S.JA, RADCHENKO I.V, GERASIMOV G.I
Format Patent
LanguageEnglish
Russian
Published 27.11.2005
Edition7
Subjects
GYROSCOPIC INSTRUMENTS
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
NAVIGATION
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHYSICS
SURVEYING
TESTING
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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