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201. http://kcor.sai.msu.ru/arXiv1002.2360.pdf
... 000, 112 (2009) Printed 11 February 2010 A (MN L TEX style file v2.2) Analytical approximations of K -corrections in optical and near-infrared bands I1gor V. Chilingarian1 2 ,2,3 , Anne-Laure Melchior 1,4 and Ivan Yu. ... Received 2010 February 01; in original form 2009 August 14 ABSTRACT To compare photometric properties of galaxies at different redshifts, the fluxes need to be corrected for the changes of effective rest-frame wavelengths of filter bandpasses, called K -corrections. ... Table 1. ...
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Ссылки http://kcor.sai.msu.ru/arXiv1002.2360.pdf -- 1631.3 Кб -- 12.02.2010
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202. Analemma
... Multiexposition 34 images Sun 1/1000 sec f/22 and 1 image background. ... It shows position of the Sun on the sky in the same time of a day during one year. Analemma - a trace of the annual movement of the Sun on the sky - is well known among experts of sun-dials and old Earth's globes as a diagram of change of seasons and an equation of time. ... Previously, the position of the Sun on the sky was calculated with computer as well as optimal moments of time for taking each of the exposures. ...
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Ссылки http://www.vrum.chat.ru/Photo/Astro/analema.htm -- 6.7 Кб -- 09.04.2016
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203. Accuracy of World positional CCD observations of the numbered minor planets
. Authors . Problem . Method . Advises . Contact Analysis of an accuracy of CCD asteroid observations carried out by professional and amateur astronomers . An accuracy estimation of CCD asteroid observations contained in the Minor Planet Center Database and carried out in the years 1999 - 2006 is realized. About 20 millions individual positions of the Numbered and Unnumbered Minor Planets were tested by means of calculations of (O-C) residuals to derive "mean error of a single observation" for more than 400
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Ссылки http://www.accuracy.puldb.ru/AYA.HTM -- 283.1 Кб -- 05.12.2007
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204. http://www.kiam1.rssi.ru/pubs/AAS_09-103.pdf
... 23 Algorithm fo r evalua tion of two burn maneuv ers using linearity Input information: ( t t E1 , rEI , v t1L , t E2 2L ( ) EI )T )T the time and the state vector of initial orbit for this time ; interval of possible thrusts for transition from initial orbit to the transfer on e; the time and the state vector of the target orbit for this time ; ... We cal culate the state vector for the initial orbit for the time t1a and the target one for the time t2 a . ...
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Ссылки http://www.kiam1.rssi.ru/pubs/AAS_09-103.pdf -- 2056.5 Кб -- 05.09.2014
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