Comet Hale-Bopp (C/1995 O1): UVSTAR-FUV Spectroscopy from the Space Shuttle     

Cristiano B. Cosmovici  Vojko Bratina  Gottfried Schwarz  Gianpaolo Tozzi  Michael J. Mumma  Roberto Stalio 《Astrophysics and Space Science》2006,301(1-4):135-143

We report here on unique post-perihelion (2.3 AU) measurements of Comet Hale-Bopp in the FUV-range (950–1250 Å) by means of the UVSTAR spectrometer from the space shuttle with the main purpose of searching for argon and other FUV emitters. New methods for separating the strong airglow emission at shuttle altitudes are here discussed in detail. Due to our low resolution (15 Å) and S/N ratio the possible rocket-borne detection of argon near perihelion (0.9 AU) could not be confirmed. New species as N₂ are suspected but difficult to separate from the strong airglow emission at shuttle altitudes. From the Lyα brightness (1.30± 0.08 kRy) a water production rate Q = 5.9 ± 0.4 × 10²⁹ molecules s^?1 could be derived and compared with other post-perihelion observations.  相似文献   

Methods and Results of an Optical Search for Extraterrestrial Civilizations     

G. Beskin  N. Borisov  V. Komarova  S. Mitronova  S. Neizvestny  V. Plokhotnichenko  M. Popova 《Astrophysics and Space Science》1997,248(1-2):51-57

I summarize fully-sampled observations of the 3 mm emission from CO and HCN in the inner arcminute of NGC 1068. The CO emission is distributed in the form of a molecular bar, coincident with the infrared bar, from which emanate two spiral arms. A relatively weak concentration of CO line emission is found at the nucleus. By contrast, the HCN emission is strongly concentrated at the center, with relatively weak emission in the region of the star-forming arms. The ratio of HCN to CO integrated intensities is about 0.6 over the central r ≉ 175 pc and is the highest ratio measured in the center of any galaxy; the ratio reflects the high thermal pressure (TK ~ 50 K, n[H2] ~ 4 × 106 cm-3) in the few hundred parsecs surrounding the nucleus. The kinematics in the star-forming arms are well described by circular orbits, with ordered noncircular motions of < 30 km s-1 that may be attributed to spiral density wave streaming. Interior to the bar, noncircular motions dominate the gas kinematics. A model of the CO kinematics contrains any Inner Lindblad Resonance to be close to the location of the hundred-parsec scale HCN ‘disk’. At the nucleus, the spatially unresolved CO emission shows a triplet velocity structure characteristic of kinematically independent regions. This revised version was published online in July 2006 with corrections to the Cover Date.  相似文献   

柴达木盆地中深层混积岩储层形成机制   总被引：10，自引：1，他引：9  

冯进来  曹剑  胡凯  陈琰  杨少勇  刘云田  边立曾  张国卿 《岩石学报》2011,27(8):2461-2472

通过岩心观测、普通薄片、铸体薄片、扫描电镜、电子探针和岩石物性等分析,系统阐述了柴达木盆地典型中深层(西北区南翼山构造E₃²-N₁)混积岩的岩石学、储集空间/物性和成岩作用等特征,在此基础上讨论了储层形成机制。结果表明,混积岩以(泥质)泥晶灰岩、钙质含量较高的砂岩和粉砂岩及其混积岩为主;储集空间以溶蚀改造的裂缝和粒间溶蚀孔隙为特征,物性总体表现为低孔-特低孔、超低渗-非渗透;有利于形成储层的成岩作用是溶蚀和构造裂缝作用;储层形成机制可归纳为"岩性是基础,裂缝是条件,溶蚀是关键"。这可为区域中深层混积岩储层,乃至陆相湖泊混合沉积储层的研究与油气勘探开发提供借鉴与参考。  相似文献   

Assessment of satellite ocean color products of MERIS,MODIS and SeaWiFS along the East China Coast (in the Yellow Sea and East China Sea)     

《ISPRS Journal of Photogrammetry and Remote Sensing》2014

The validation of satellite ocean-color products is an important task of ocean-color missions. The uncertainties of these products are poorly quantified in the Yellow Sea (YS) and East China Sea (ECS), which are well known for their optical complexity and turbidity in terms of both oceanic and atmospheric optical properties. The objective of this paper is to evaluate the primary ocean-color products from three major ocean-color satellites, namely the Moderate Resolution Imaging Spectroradiometer (MODIS), Medium Resolution Imaging Spectrometer (MERIS), and Sea-viewing Wide Field-of-view Sensor (SeaWiFS). Through match-up analysis with in situ data, it is found that satellite retrievals of the spectral remote sensing reflectance R_rs(λ) at the blue-green and green bands from MERIS, MODIS and SeaWiFS have the lowest uncertainties with a median of the absolute percentage of difference (APD_m) of 15–27% and root-mean-square-error (RMS) of 0.0021–0.0039 sr⁻¹, whereas the R_rs(λ) uncertainty at 412 nm is the highest (APD_m 47–62%, RMS 0.0027–0.0041 sr⁻¹). The uncertainties of the aerosol optical thickness (AOT) τ_a, diffuse attenuation coefficient for downward irradiance at 490 nm K_d(490), concentrations of suspended particulate sediment concentration (SPM) and Chlorophyll a (Chl-a) were also quantified. It is demonstrated that with appropriate in-water algorithms specifically developed for turbid waters rather than the standard ones adopted in the operational satellite data processing chain, the uncertainties of satellite-derived properties of K_d(490), SPM, and Chl-a may decrease significantly to the level of 20–30%, which is true for the majority of the study area. This validation activity advocates for (1) the improvement of the atmosphere correction algorithms with the regional aerosol optical model, (2) switching to regional in-water algorithms over turbid coastal waters, and (3) continuous support of the dedicated in situ data collection effort for the validation task.  相似文献   

基于GPU的S63标准电子海图数据解密算法     

钟云海  郑海  周红进 《测绘软科学研究》2014,(2):54-58

S63标准采用Blowfish算法对原始海图数据加密后发行,数据的解密成为电子海图系统数据转换和更新中一个耗时的过程。为提高数据处理的速度,针对Blowfish分组密码算法的特点,提出一种利用图形处理器（GPU）的海图并行解密算法,并采用数据传输和处理的同步技术进行了优化。测试表明,采用GPU的并行解密算法是纯CPU串行处理的9.8倍。该算法不仅可大大加快海图数据转换和更新过程,对地理信息系统海量数据处理也有一定的借鉴价值。  相似文献   

Mohr Space in Andersonian Stress State and Its Application in Active Fault     

TONG Hengmao 《《地质学报》英文版》2013,87(Z1):387-387

  相似文献   

云南铁矿资源现状及扩大远景途径     

杨宁  薛步高 《云南地质》2013,(4):389-392

全省上表铁矿111处,总储量32.16亿吨,其中有11.27亿吨暂不能使用.而且,富铁矿少,难选矿多,分布边远,难以满足经济发展需求.必须解决菱铁矿、高磷矿选矿问题,以及有远景磁异常补充深部找矿问题,可望取得突破.  相似文献   

Trajectory Analysis and Design for A Jupiter Exploration Mission   总被引：1，自引：0，他引：1  

Chen Yang  Baoyin He-xiLi Jun-feng 《Chinese Astronomy and Astrophysics》2013

The trajectory design for a Jupiter exploration mission is investigated in this paper. The differences between the Jupiter exploration trajectory and the Mars or Venus exploration trajectory are mainly concerned about. Firstly, the selection of the Jupiter-centered orbit is analyzed based on the Galileo Jupiter mission. As for the Earth-Jupiter transfer orbit, the fuel consumption of the direct transfer is too large. So the energy-saving technologies such as the planetary gravity assist should be used for the trajectory to the Jupiter. The different sequences of planetary gravity assists are examined by applying the Particle Swarm Optimization (PSO). According to the searched result, the Venus-Earth-Earth sequence (VEEGA) is the most effective one for the Jupiter mission. During the Jupiter mission, the spacecraft will pass though the main asteroid belt between the orbits of Mars and Jupiter, and may encounter multiple asteroids. Therefore the Jupiter mission is able to combine with the main-belt asteroid flyby mission. The design method of the intermediate asteroid flyby trajectory is also considered. At last, an entire trajectory for the Jupiter mission launched in 2023 is presented.  相似文献   

The Bootstrap Estimation of the Accuracy of Preliminary Orbit Determination     

Wang Xin 《Chinese Astronomy and Astrophysics》2013

From the point of view of the non-parametric statistics, a general estimation method of the accuracy and con?dence interval of preliminary orbit determination is proposed for the occasion without any other information but observational data. Based on the bootstrap method, the estimation relies only on the observational data and does not require the precise orbit determination as a reference, or the assumption of normal distribution of observational errors. Numerical experiments show that this method is very simple in implementa- tion, and may serve as an easy accuracy evaluation for the preliminary orbit determination and for the follow-up employments.  相似文献   

Optimization of Low-Thrust Trajectories Using an Indirect Shooting Method without Guesses of Initial Costates     

Lin Hou-yuan  Zhao Chang-yin 《Chinese Astronomy and Astrophysics》2012

According to the optimal control theory, the optimal control problem of the low-thrust tra jectory can be converted into a solution of nonlinear two- point boundary-value problem (TPBVP). To solve the TPBVP, the repeated random guesses for the initial costate variables and iterative computations are needed. In order to enhance the convergence of the iterations, we select an appropriate performance index, and then linearize the equations of the TPBVP around a Keplerian orbit. For multi-revolution transfers, instead of the multi- revolution Lambert tra jectory, multiple segmented Keplerian arcs are used to ensure the effectiveness of the linearization. The method is totally automatic with multiple iterations. With this method, we can get the results within 3 ∼ 5 iterations, and the random guess of the initial costates is unnecessary. Finally by the iterative optimization of the performance index, a better control strategy approaching to the bang-bang control is obtained.  相似文献