Äîêóìåíò âçÿò èç êýøà ïîèñêîâîé ìàøèíû. Àäðåñ îðèãèíàëüíîãî äîêóìåíòà : http://www.cosmos.ru/eng/2014niokr.pdf Äàòà èçìåíåíèÿ: Mon Feb 16 19:40:13 2015 Äàòà èíäåêñèðîâàíèÿ: Sun Apr 10 02:52:15 2016 Êîäèðîâêà: Ïîèñêîâûå ñëîâà: ï ï ï ï ï ï ï ï ï ï ï ï ï ï ï ï ï ï ï ï ï ð ï ð ï ð ï ð ï

Main research and development work completed in 2014 and ready for implementation 1. VEGA-GEOGLAM Information System for Global Agricultu re Monitoring using Earth Observation Satellites Space Research Institute of Russian Academy o f Sciences Dr.Sc. Loupian E. A., Dr.Sc. Bartalev S. A. Informat ion system VEGA-GEOGLAM (http://vega.geoglam.ru/) was developed by IKI to support init iated by the G20 countries GEOGLAM programme on creation of global system for satellit e monit oring of agriculture. The VEGA-GEOGLAM system allows near-real-t ime analysis o f the Earth observat ion satellit e data regularly acquiring over globally distributed test sites in different countries of Eurasia, Africa, North and South America to monitor status of different agricultural crops and harvest forecast. The system permits to develop agr icultural satellit e monitoring capacit y in d ifferent regions of t he World.

The test-sites (marked in red) network for agricult ural monitoring using Earth observat ion satellite data based o n the VEGA-GEOGLAM information syst em The VEGA-GEOGLAM development was supported by the Russian Academy o f Sciences and the SIGMA project funded by t he European Co mmission. 2. MicroBOKZ - the New Generation Star Tracker The new generat ion miniature star tracker MicroBOKZ was developed at IKI RAN in 2014. This device was installed on the small spacecraft "Aurora" and launched into space on June 06, 2014. MicroBOKZ star tracker exceeds both the Russian and foreign analo gues in dimensio ns, weight and accuracy characterist ics. The tracker has a mass o f 600 g, power consumpt ion of 1 W and provides for measuring the optical axis orientation parameters with a rando m error of less t han 1 arcsec. The star trackers MicroBOKZ and BOKZM60/1000 are shown in fig. 1. These devices have a similar accuracy but differ in weight and power consumption by an order of magnitude.

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Fig. 1. Photos of star trackers (right ­ BOKZM60/1000, left ­ MicroBOKZ on CMOS Developers:

Fig. 2. Flex-rigid board of the MicroBOKZ star tracker

Avanesov G.A., Bessonov R.V., Dyat lov S.A., Zaretskaya E.V., Karavayeva E.S., Krasikov V.A., Mysnik E.A., Prokhorova S.A., Filippova O.V., Forsch A. A. Scient ific and technical materials: 1. G.A. Avanesov, R.V. Bessonov, A.A. Forsch, R.G. Zalyalo va, A.V. Filatov «Operating experience and prospects of the BOKZ star trackers development». The 4th All-Russian Scient ific and Technical Conference "Contemporary Problems of Spacecraft Orientation and Navigation ", Tarusa, 8­11 September 2014 Abstracts. IKI, 2014, P. 3. G.A. Avanesov, R.V. Bessonov, S.A. Dyatlov, E.A. Mysnik «Ground t esting of the MicroBOKZ star trackers». The 4th All-Russian Scient ific and Technical Conference "Contemporar y Problems of Spacecraft Orientation and Navigat ion ", Tarusa, 8­11 September 2014 Abstracts. IKI, 2014, P. 8-9. G.A. Avanesov, R.V. Bessonov, A.A. Forsch, M.I. Kudelin «Analys is of current state and prospects of the BOKZ family star trackers development». «Pr iborostroenie», submitted for publicat ion. Scient ific&Technical report "Study on the orientatio n device in t he field of stars as regards testing of t he radiat ion detectors, microprocessor devices and built-in angular velocit y sensors; device operation simulat ion; modeling and mocking-up bench equipment for testing instruments", 2013

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