Utilization of Inertial Reference Unit in the Structure of a Free Space Optical Link

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F12%3A00476876" target="_blank" >RIV/60162694:G43__/12:00476876 - isvavai.cz</a>

Result on the web

<a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Utilization of Inertial Reference Unit in the Structure of a Free Space Optical Link

Original language description

The paper deals with the design of a control system for a mobile free-space optical link. Basic conditions of the system operation are described. These conditions are a variable steady model and permissible fluctuations of the received optical power. They dictate limit angular deflections of optical axes of link stations. On the basis of the deflections a design and features of a system of the axes position control have to be specified. The inertial reference unit (IRU) is an important part of the angular position control system. The small and simple IRU uses inertial sensors based on the MEMS technology.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

KA - Militarism

OECD FORD branch

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Project

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Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2012

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection

New Trends in Aviation Development

ISBN

978-80-553-1083-1

ISSN

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e-ISSN

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Number of pages

4

Pages from-to

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Publisher name

Faculty of Aeronautics, Technical University of Košice

Place of publication

Košice

Event location

Košice

Event date

Jan 1, 2012

Type of event by nationality

EUR - Evropská akce

UT code for WoS article

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