Ural serkan (6 resultados)

Taschenbuch. Condición: Neu. Near Real Time Orbit Determination of Bilsat-1 | Exploring Algorithms | Serkan Ural (u. a.) | Taschenbuch | 88 S. | Englisch | 2010 | LAP LAMBERT Academic Publishing | EAN 9783838389721 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. …

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Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Artificial satellites are integrated with a wide area of applications expanding with a new contribution every day. The need for knowing the satellite's state at a specific instant of time with variable accuracy requirements depending on the purpose exists for all artificial satellites. A variety of techniques has emerged since the first satellite launched to its orbit and more techniques will surely be involved as far as the pursuit of higher efficiency exists. There are various orbit determination strategies in which the GPS observables are involved. This book investigates different algorithms using the data from the GPS receiver on board the first Turkish remote sensing micro-satellite BilSAT-1. Pseudorange observations of BilSAT-1 obtained from TÜB TAK-UZAY are used to perform different orbit determination algorithms. Both a kinematic orbit determination approach with least squares estimation on the basis of Gauss- Markoff model and reduced-dynamic orbit determination approach with Kalman filter estimation algorithms are investigated to explore the affects of variations in the algorithms. 88 pp. Englisch.…

Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Ural SerkanSerkan Ural is a research assistant in Department of Geodesy and Photogrammetry Engineering at Hacettepe University. Mahmut O. Karslioglu is an associate professor in Geomatics Division, Civil Engineering Department and.…

Taschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Artificial satellites are integrated with a wide area of applications expanding with a new contribution every day. The need for knowing the satellite''s state at a specific instant of time with variable accuracy requirements depending on the purpose exists for all artificial satellites. A variety of techniques has emerged since the first satellite launched to its orbit and more techniques will surely be involved as far as the pursuit of higher efficiency exists. There are various orbit determination strategies in which the GPS observables are involved. This book investigates different algorithms using the data from the GPS receiver on board the first Turkish remote sensing micro-satellite BilSAT-1. Pseudorange observations of BilSAT-1 obtained from TÜB¿TAK-UZAY are used to perform different orbit determination algorithms. Both a kinematic orbit determination approach with least squares estimation on the basis of Gauss- Markoff model and reduced-dynamic orbit determination approach with Kalman filter estimation algorithms are investigated to explore the affects of variations in the algorithms.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 88 pp. Englisch.…

Taschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Artificial satellites are integrated with a wide area of applications expanding with a new contribution every day. The need for knowing the satellite's state at a specific instant of time with variable accuracy requirements depending on the purpose exists for all artificial satellites. A variety of techniques has emerged since the first satellite launched to its orbit and more techniques will surely be involved as far as the pursuit of higher efficiency exists. There are various orbit determination strategies in which the GPS observables are involved. This book investigates different algorithms using the data from the GPS receiver on board the first Turkish remote sensing micro-satellite BilSAT-1. Pseudorange observations of BilSAT-1 obtained from TÜB TAK-UZAY are used to perform different orbit determination algorithms. Both a kinematic orbit determination approach with least squares estimation on the basis of Gauss- Markoff model and reduced-dynamic orbit determination approach with Kalman filter estimation algorithms are investigated to explore the affects of variations in the algorithms.…