Title of article :
Creation of the new industry-standard space test of laser retroreflectors for the GNSS and LAGEOS Original Research Article
Author/Authors :
S. Agnello، نويسنده , , G.O. Delle Monache، نويسنده , , D.G. Currie، نويسنده , , R. Vittori، نويسنده , , M. C. Cantone، نويسنده , , M. Garattini، نويسنده , , A. Boni، نويسنده , , M. Martini، نويسنده , , C. Lops، نويسنده , , N. Intaglietta، نويسنده , , R. Tauraso، نويسنده , , D.A. Arnold، نويسنده , , M.R. Pearlman، نويسنده , , G. Bianco، نويسنده , , S. Zerbini، نويسنده , , M. Maiello، نويسنده , , S. Berardi، نويسنده , , L. Porcelli، نويسنده , , C.O. Alley، نويسنده , , J.F. McGa، نويسنده ,
Issue Information :
دوهفته نامه با شماره پیاپی سال 2011
Pages :
21
From page :
822
To page :
842
Abstract :
We built a new experimental apparatus (the “Satellite/lunar laser ranging Characterization Facility”, SCF) and created a new test procedure (the SCF-Test) to characterize and model the detailed thermal behavior and the optical performance of cube corner laser retroreflectors in space for industrial and scientific applications. The primary goal of these innovative tools is to provide critical design and diagnostic capabilities for Satellites Laser Ranging (SLR) to Galileo and other GNSS (Global Navigation Satellite System) constellations. The capability will allow us to optimize the design of GNSS laser retroreflector payloads to maximize ranging efficiency, to improve signal-to-noise conditions in daylight and to provide pre-launch validation of retroreflector performance under laboratory-simulated space conditions. Implementation of new retroreflector designs being studied will help to improve GNSS orbits, which will then increase the accuracy, stability, and distribution of the International Terrestrial Reference Frame (ITRF), to provide better definition of the geocenter (origin) and the scale (length unit).Our key experimental innovation is the concurrent measurement and modeling of the optical Far Field Diffraction Pattern (FFDP) and the temperature distribution of the SLR retroreflector payload under thermal conditions produced with a close-match solar simulator. The apparatus includes infrared cameras for non-invasive thermometry, thermal control and real-time movement of the payload to experimentally simulate satellite orientation on orbit with respect to both solar illumination and laser interrogation beams. These unique capabilities provide experimental validation of the space segment for SLR and Lunar Laser Ranging (LLR).
Keywords :
Laser retroreflectors , Industry-standard , LAGEOS , Galileo , GPS , New space test , SLR
Journal title :
Advances in Space Research
Serial Year :
2011
Journal title :
Advances in Space Research
Record number :
1133288
Link To Document :
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