Synergic application of advanced modelling methods to space antenna design

Author(s):  
A. Freni ◽  
S. Maci ◽  
G. Vecchi ◽  
M. Bandinelli ◽  
F. Mioc ◽  
...  
2017 ◽  
Vol 45 (12) ◽  
pp. 1007-1012
Author(s):  
Nam Seo Goo ◽  
Van Luong Le ◽  
Yongsan An ◽  
Woong-Ryeol Yu ◽  
Jin Ok Hwang ◽  
...  

2006 ◽  
Vol 532-533 ◽  
pp. 929-932
Author(s):  
Yong Xiao ◽  
San Min Wang ◽  
Guo Ding Chen

The technique of collaborative design and manufacture is not only very important, but also urgent necessary for space antenna. Building on unicode, XML provides the standard format describing data in various types, so it has the virtue of integrating heterogeneous databases. In this paper, the elementary research has been done on XML-based integrating technique for heterogeneous databases of space antenna. Firstly, the overall flow for collaborative design and manufacture of space antenna shows that five databases should be integrated. Secondly, a XML-based integration system frame is conceived for space antenna databases. Thirdly, an effective XML-based transformation mechanism is proposed for the data integration process between relational database and document-based database. Finally, the implement of XML-based database integration is demonstrated in a space antenna design.


1997 ◽  
Vol 161 ◽  
pp. 761-776 ◽  
Author(s):  
Claudio Maccone

AbstractSETI from space is currently envisaged in three ways: i) by large space antennas orbiting the Earth that could be used for both VLBI and SETI (VSOP and RadioAstron missions), ii) by a radiotelescope inside the Saha far side Moon crater and an Earth-link antenna on the Mare Smythii near side plain. Such SETIMOON mission would require no astronaut work since a Tether, deployed in Moon orbit until the two antennas landed softly, would also be the cable connecting them. Alternatively, a data relay satellite orbiting the Earth-Moon Lagrangian pointL2would avoid the Earthlink antenna, iii) by a large space antenna put at the foci of the Sun gravitational lens: 1) for electromagnetic waves, the minimal focal distance is 550 Astronomical Units (AU) or 14 times beyond Pluto. One could use the huge radio magnifications of sources aligned to the Sun and spacecraft; 2) for gravitational waves and neutrinos, the focus lies between 22.45 and 29.59 AU (Uranus and Neptune orbits), with a flight time of less than 30 years. Two new space missions, of SETI interest if ET’s use neutrinos for communications, are proposed.


PIERS Online ◽  
2007 ◽  
Vol 3 (7) ◽  
pp. 1067-1070 ◽  
Author(s):  
Wenwen Chai ◽  
Xiaojuan Zhang ◽  
Jibang Liu

2017 ◽  
Vol 49 (004) ◽  
pp. 767--772
Author(s):  
G. AHMAD ◽  
M. I. BABAR ◽  
M. IRFAN ◽  
M. ASHRAF ◽  
T. JAN

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