DocumentCode :
1928015
Title :
VLBI tracking of the solar sail mission IKAROS
Author :
Takeuchi, H. ; Horiuchi, S. ; Phillips, C. ; Edwards, P. ; McCallum, J. ; Ellingsen, S. ; Dickey, J. ; Ichikawa, R. ; Takefuji, K. ; Yamaguchi, T. ; Kurihara, S. ; Ichikawa, B. ; Yoshikawa, M. ; Tomiki, A. ; Sawada, H. ; Jinsong, P.
Author_Institution :
JAXA, Sagamihara, Japan
fYear :
2011
fDate :
13-20 Aug. 2011
Firstpage :
1
Lastpage :
4
Abstract :
IKAROS (Interplanetary Kite-craft Accelerated by Radiation Of the Sun) is the world´s first spacecraft to successfully demonstrate solar-sail technology in interplanetary space. The spacecraft is made of square shape of very thin membrane, whose diagonal dimension is 20m. By changing its attitude toward Sun, radiation pressure of solar photons can be used as propulsive force of the spacecraft. To determine the orbit under the continuous big influence of the nongravitational perturbative force (i.e. solar radiation pressure), Very Long Baseline Interferometry (VLBI) observation is effective because sky plane position of the spacecraft can be directly and instantaneously measured by VLBI observables without (or with less dependence on) a priori assumption for solar radiation pressure model. In order to effectively perform VLBI measurements, a signal generator of Differential One-way Range (DOR) tones, which consist of multiple tones whose spanning bandwidth is about 28MHz, was developed and installed to the spacecraft. A digital backend system for the ground stations which has maximum output performance of 4-Gbps had also developed to sample wideband DOR tones. A total number of 24 international VLBI experiments were carried out by using totally 15 antennas among 8 agencies during July and August in 2010. As a result of initial analysis, measurement accuracy of VLBI delay was confirmed to be 50 pico second level, which is 20 times improved precision compared to the JAXA´s conventional deep space spacecraft such as Hayabusa and Akatsuki.
Keywords :
aerospace propulsion; astronomical instruments; radiation pressure; radioastronomical techniques; radiowave interferometry; signal generators; space vehicles; Akatsuki deep space spacecraft; Hayabusa deep space spacecraft; IKAROS; JAXA; VLBI delay; VLBI observables; VLBI tracking; Very Long Baseline Interferometry observation; diagonal dimension; differential one-way range tones; digital backend system; international VLBI experiments; interplanetary space; maximum output performance; measurement accuracy; nongravitational perturbative force; signal generator; sky plane position; solar photons; solar radiation pressure model; solar sail mission; solar-sail technology; wideband DOR tones; Delay; Extraterrestrial measurements; Solar radiation; Space missions; Space vehicles; Wideband;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
General Assembly and Scientific Symposium, 2011 XXXth URSI
Conference_Location :
Istanbul
Print_ISBN :
978-1-4244-5117-3
Type :
conf
DOI :
10.1109/URSIGASS.2011.6051213
Filename :
6051213
Link To Document :
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