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961.
简要对比DDN、SDH光纤、卫星和无线CDMA等几种通讯方式的优缺点,介绍重庆区域测震台网所使用的传输方案,即以SDH光纤传输为主、无线CDMA为辅的双链路备份传输方案。重点介绍该传输方案的原理和实施方法,详细讲述台站及台网中心的路由配置和相关说明。通过在重庆市区域测震台网的运行,结果发现,传输效果较理想,测震台网台站运行率均达到98%以上,证明了该方案应用的可行性。 相似文献
962.
Mark Clampin Marco Sirianni George F. Hartig Holland C. Ford Garth D. Illingworth Bill Burmester William Koldewynd Andre R. Martel Adam Riess Ronald J. Schrein Pamela C. Sullivan 《Experimental Astronomy》2002,14(2):107-115
The Advanced Camera for Surveys (ACS), installed in the Hubble Space telescope in March 2002, will significantly extend HST's
deep, survey imaging capabilities. ACS has met, or exceeded, all of its key performance specifications. In this paper we briefly
review the in-flight performance of the instrument's CCD detectors and preview early ACS science observations.
This revised version was published online in July 2006 with corrections to the Cover Date. 相似文献
963.
T. Appourchaux P. Liewer M. Watt D. Alexander V. Andretta F. Auchère P. D’Arrigo J. Ayon T. Corbard S. Fineschi W. Finsterle L. Floyd G. Garbe L. Gizon D. Hassler L. Harra A. Kosovichev J. Leibacher M. Leipold N. Murphy M. Maksimovic V. Martinez-Pillet B. S. A. Matthews R. Mewaldt D. Moses J. Newmark S. Régnier W. Schmutz D. Socker D. Spadaro M. Stuttard C. Trosseille R. Ulrich M. Velli A. Vourlidas C. R. Wimmer-Schweingruber T. Zurbuchen 《Experimental Astronomy》2009,23(3):1079-1117
The POLAR Investigation of the Sun (POLARIS) mission uses a combination of a gravity assist and solar sail propulsion to place
a spacecraft in a 0.48 AU circular orbit around the Sun with an inclination of 75° with respect to solar equator. This challenging
orbit is made possible by the challenging development of solar sail propulsion. This first extended view of the high-latitude
regions of the Sun will enable crucial observations not possible from the ecliptic viewpoint or from Solar Orbiter. While
Solar Orbiter would give the first glimpse of the high latitude magnetic field and flows to probe the solar dynamo, it does
not have sufficient viewing of the polar regions to achieve POLARIS’s primary objective: determining the relation between
the magnetism and dynamics of the Sun’s polar regions and the solar cycle.
相似文献
T. AppourchauxEmail: |
964.
Triple F—a comet nucleus sample return mission 总被引:1,自引:0,他引:1
《Experimental Astronomy》2009,23(3):809-847
The Triple F (Fresh From the Fridge) mission, a Comet Nucleus Sample Return, has been proposed to ESA’s Cosmic Vision program. A sample return from a comet
enables us to reach the ultimate goal of cometary research. Since comets are the least processed bodies in the solar system,
the proposal goes far beyond cometary science topics (like the explanation of cometary activity) and delivers invaluable information
about the formation of the solar system and the interstellar molecular cloud from which it formed. The proposed mission would
extract three sample cores of the upper 50 cm from three locations on a cometary nucleus and return them cooled to Earth for
analysis in the laboratory. The simple mission concept with a touch-and-go sampling by a single spacecraft was proposed as
an M-class mission in collaboration with the Russian space agency ROSCOSMOS. 相似文献
965.
European Venus Explorer (EVE): an in-situ mission to Venus 总被引:1,自引:0,他引:1
E. Chassefière O. Korablev T. Imamura K. H. Baines C. F. Wilson D. V. Titov K. L. Aplin T. Balint J. E. Blamont C. G. Cochrane Cs. Ferencz F. Ferri M. Gerasimov J. J. Leitner J. Lopez-Moreno B. Marty M. Martynov S. V. Pogrebenko A. Rodin J. A. Whiteway L. V. Zasova J. Michaud R. Bertrand J.-M. Charbonnier D. Carbonne P. Raizonville 《Experimental Astronomy》2009,23(3):741-760
The European Venus Explorer (EVE) mission was proposed to the European Space Agency in 2007, as an M-class mission under the
Cosmic Vision Programme. Although it has not been chosen in the 2007 selection round for programmatic reasons, the EVE mission
may serve as a useful reference point for future missions, so it is described here. It consists of one balloon platform floating
at an altitude of 50–60 km, one descent probe provided by Russia, and an orbiter with a polar orbit which will relay data
from the balloon and descent probe, and perform science observations. The balloon type preferred for scientific goals is one
which oscillates in altitude through the cloud deck. To achieve this flight profile, the balloon envelope contains a phase
change fluid, which results in a flight profile which oscillates in height. The nominal balloon lifetime is 7 days—enough
for one full circumnavigation of the planet. The descent probe’s fall through the atmosphere takes 60 min, followed by 30 min
of operation on the surface. The key measurement objectives of EVE are: (1) in situ measurement from the balloon of noble
gas abundances and stable isotope ratios, to study the record of the evolution of Venus; (2) in situ balloon-borne measurement
of cloud particle and gas composition, and their spatial variation, to understand the complex cloud-level chemistry; (3) in
situ measurements of environmental parameters and winds (from tracking of the balloon) for one rotation around the planet,
to understand atmospheric dynamics and radiative balance in this crucial region. The portfolio of key measurements is complemented
by the Russian descent probe, which enables the investigation of the deep atmosphere and surface. 相似文献
966.
SGP4/SDP4模型精度分析 总被引:2,自引:0,他引:2
本文基于最新发布的SGP4/SDP4(Simplified General Perturbation Version 4/Simplified Deep-space Perturbation Version 4)模型设计了一套定轨方案,从空间目标库中挑选出不同类型和轨道参数的1120个目标进行计算,定量给出了SGP4/SDP4模型处理不同类型空间目标的定轨预报精度.结果表明:近地目标定轨精度为百米量级;半同步和同步轨道定轨精度平均为0.7和1.9km.椭圆轨道目标的定轨精度与偏心率有关,除少数e>0.8的椭圆轨道目标,绝大多数椭圆轨道目标定轨误差均小于10km.用SGP4/SDP4模型对近地目标预报3天,半同步轨道预报30天,同步轨道预报15天,椭圆轨道预报1天,预报误差一般不超过40km. 相似文献
967.
G. Amelino-Camelia K. Aplin M. Arndt J. D. Barrow R. J. Bingham C. Borde P. Bouyer M. Caldwell A. M. Cruise T. Damour P. D’Arrigo H. Dittus W. Ertmer B. Foulon P. Gill G. D. Hammond J. Hough C. Jentsch U. Johann P. Jetzer H. Klein A. Lambrecht B. Lamine C. Lämmerzahl N. Lockerbie F. Loeffler J. T. Mendonca J. Mester W.-T. Ni C. Pegrum A. Peters E. Rasel S. Reynaud D. Shaul T. J. Sumner S. Theil C. Torrie P. Touboul C. Trenkel S. Vitale W. Vodel C. Wang H. Ward A. Woodgate 《Experimental Astronomy》2009,23(2):549-572
The GAUGE (GrAnd Unification and Gravity Explorer) mission proposes to use a drag-free spacecraft platform onto which a number
of experiments are attached. They are designed to address a number of key issues at the interface between gravity and unification
with the other forces of nature. The equivalence principle is to be probed with both a high-precision test using classical
macroscopic test bodies, and, to lower precision, using microscopic test bodies via cold-atom interferometry. These two equivalence
principle tests will explore string-dilaton theories and the effect of space–time fluctuations respectively. The macroscopic
test bodies will also be used for intermediate-range inverse-square law and an axion-like spin-coupling search. The microscopic
test bodies offer the prospect of extending the range of tests to also include short-range inverse-square law and spin-coupling
measurements as well as looking for evidence of quantum decoherence due to space–time fluctuations at the Planck scale. 相似文献
968.
Alessandro Rossi 《Celestial Mechanics and Dynamical Astronomy》2008,100(4):267-286
The Medium Earth Orbit region is the home of the navigation constellations. It is shown how the orbits of these constellations
of satellites are strongly affected by the so-called inclination dependent luni-solar resonances. The analytical theory of
these resonances is recalled and a large set of numerical integrations is used to investigate the stability of the orbits
of the constellations over very long time spans. The stability issue is important in the definition of possible disposal strategies
for the constellation spacecraft, after their end-of-life. Two possible disposal strategies are envisaged involving either
stable or unstable orbits (from the eccentricity growth point of view). In particular it is shown how, to have disposal orbits
with moderately short lifetime (of the orders of 40–50 years), a very large disposal maneuver would be required to rise the
inital eccentricity to values above ~ 0.3. 相似文献
969.
A model is presented that describes the excitation of small-scale density perturbations and electromagnetic fields by standing shear Alfvén waves in a Cartesian geometry. The model includes the effects of plasma betas and the Hall term effects. The characteristics of magnetospheric density cavities and the formation of the significant peak in density are discussed in the paper. 相似文献
970.
E. L. Wright 《New Astronomy Reviews》2003,47(11-12):877
The Wilkinson Microwave Anisotropy Probe (WMAP) science team has released results from the first year of operation at the Earth–Sun L2 Lagrange point. The maps are consistent with previous observations but have much better sensitivity and angular resolution than the COBE DMR maps, and much better calibration accuracy and sky coverage than ground-based and balloon-borne experiments. The angular power spectra from these ground-based and balloon-borne experiments are consistent within their systematic and statistical uncertainties with the WMAP results. WMAP detected the large angular-scale correlation between the temperature and polarization anisotropies of the CMB caused by electron scattering since the Universe became reionized after the “Dark Ages”, giving a value for the electron scattering optical depth of 0.17 ± 0.04. The simplest ΛCDM model with n=1 and Ωtot=1 fixed provides an adequate fit to the WMAP data and gives parameters which are consistent with determinations of the Hubble constant and observations of the accelerating Universe using supernovae. The time-ordered data, maps, and power spectra from WMAP can be found at http://lambda.gsfc.nasa.gov along with 13 papers by the WMAP science team describing the results in detail. 相似文献