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91.
Sergio Fabiani Enrico CostaRonaldo Bellazzini Alessandro BrezSergio Di Cosimo Francesco LazzarottoFabio Muleri Alda RubiniPaolo Soffitta Gloria Spandre 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012,49(1):143-149
The Sun is the nearest astrophysical source with a very intense emission in the X-ray band. The study of energetic events, such as solar flares, can help us to understand the behaviour of the magnetic field of our star. There are in the literature numerous studies published about polarization predictions, for a wide range of solar flares models involving the emission from thermal and/or non-thermal processes, but observations in the X-ray band have never been exhaustive.The gas pixel detector (GPD) was designed to achieve X-ray polarimetric measurements as well as X-ray images for far astrophysical sources. Here we present the possibility to employ this instrument for the observation of our Sun in the X-ray band. 相似文献
92.
93.
L. Di Fino V. ZaconteA. Ciccotelli M. LarosaL. Narici 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Active detectors used as radiation monitors in space are not usually able to perform Particle Identification (PID). Common techniques need energy loss spectra with high statistics to estimate ion abundances. The ALTEA-space detector system is a set of silicon strip particle telescopes monitoring the radiation environment on board the International Space Station since July 2006 with real-time telemetry capabilities. Its large geometrical factor due to the concurrent use of six detectors permits the acquisition of good energy loss spectra even in a short period of observation. In this paper we present a novel Fast Probabilistic Particle Identification (FPPI) algorithm developed for the ALTEA data analysis in order to perform nuclear identification with low statistics and, with some limitations, also in real time. 相似文献
94.
W. Menn O. Adriani G.C. Barbarino G.A. Bazilevskaya R. Bellotti M. Boezio E.A. Bogomolov L. Bonechi M. Bongi V. Bonvicini S. Borisov S. Bottai A. Bruno F. Cafagna D. Campana R. Carbone P. Carlson M. Casolino G. Castellini L. Consiglio M.P. De Pascale C. De Santis N. De Simone V. Di Felice A.M. Galper W. Gillard L. Grishantseva G. Jerse A.V. Karelin S.V. Koldashov S.Y. Krutkov A.N. Kvashnin A. Leonov V. Malakhov V. Malvezzi L. Marcelli A.G. Mayorov V.V. Mikhailov E. Mocchiutti A. Monaco N. Mori N. Nikonov G. Osteria F. Palma P. Papini M. Pearce P. Picozza C. Pizzolotto M. Ricci S.B. Ricciarini 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
95.
Zenith Pass Problem of Inter-satellite Linkage Antenna Based on Program Guidance Method 总被引:1,自引:0,他引:1
Zhai Kun Yang Di 《中国航空学报》2008,21(1):53-60
While adopting an elevation-over-azimuth architecture by an inter-satellite linkage antenna of a user satellite, a zenith pass problem always occurs when the antenna is tracing the tracking and data relay satellite (TDRS). This paper deals with this problem by way of, firstly, introducing movement laws of the inter-satellite linkage to predict the movement of the user satellite antenna followed by analyzing the potential pass moment and the actual one of the zenith pass in detail. A number of specific orbit altitudes for the user satellite that can remove the blindness zone are obtained. Finally, on the base of the predicted results from the movement laws of the inter-satellite linkage, the zenith pass tracing strategies for the user satellite antenna are designed under the program guidance using a trajectory preprocessor. Simulations have confirmed the reasonability and feasibility of the strategies in dealing with the zenith pass problem. 相似文献
96.
以对转压气机为研究对象,在数值方法校验的基础上,应用全通道定常流场分析手段计算了对转压气机不同周向畸变条件下的三维流场,获取了周向总压进气畸变对该压气机性能以及流场结构的影响效应,确定了对转压气机的临界畸变角,分析了不同畸变强度对压气机性能的影响规律,探讨了周向总压畸变在对转压气机中的发展演化过程。结果表明:(a)所研究的对转压气机临界畸变角约为72°,略高于传统动-静叶排交替的压气机临界畸变角;(b)相比均匀进气工况,当畸变指数为0.24时,对转压气机失速点压比和失速裕度分别下降3%和9.6%,当畸变指数为0.5时二者分别下降8.3%和19.8%;(c)未畸变区与畸变区流体之间存在的压力梯度影响转子叶片相对来流速度。进入畸变区叶片来流相对速度减小,负荷降低,退出畸变区叶片来流相对速度增大,负荷增大;(d)上游转子使得畸变水平提高,下游转子反向旋转效应抑制了来流相对速度变化趋势,增强了气流在其叶片通道中的掺混,使得畸变水平有所下降。 相似文献
97.
98.
V. Bianchin L. Foschini G. Di Cocco F. Gianotti D. Götz P. Laurent G. Malaguti F. Schiavone 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
We present the preliminary results of a systematic search for GRB and other transients in the publicly available data for the IBIS/PICsIT (0.2–10 MeV) detector on board INTEGRAL. Lightcurves in 2–8 energy bands with time resolution from 1 to 62.5 ms have been collected and an analysis of spectral and temporal characteristics has been performed. This is the nucleus of a forthcoming first catalog of GRB observed by PICsIT. 相似文献
99.
对超高频(UHF)波段多通道合成孔径雷达(SAR)动目标检测技术进行研究,解决了长相干积累时间导致动目标在方位向散焦严重的问题。采用分块自聚焦技术对多通道SAR地面移动目标指示(GMTI)系统自适应杂波抑制后的SAR图像进行处理,改善杂波抑制后的SAR图像中动目标的聚焦情况,增强动目标与周围剩余杂波的对比度,进而提高恒虚警率(CFAR)检测的性能。与传统杂波抑制后直接进行CFAR检测方法相比较,该方法降低了检测虚警概率。实测数据处理结果显示动目标的信杂比明显提高,动目标方位向聚焦成功,证明了该方法的有效性。 相似文献
100.
为了研究叶轮机叶片的失速颤振特性,发展了一种计算流体力学与计算结构力学(CFD/CSD)时域耦合方法。该方法通过每一物理时刻CFD和CSD的循环迭代实现了耦合计算。在CFD分析中,采用鲁棒性较好的空间离散格式AUSM+-UP,并基于延迟脱体涡模型(DDES)模拟了带分离流动。在结构分析中,通过模态法构建了旋转叶片动力学方程并运用杂交多步方法进行求解。以孤立转子Rotor37为例,计算了不同工况下流场总体与细节参数,与实验结果的对比验证了CFD算法的精度。对某转子叶片进行了颤振特性研究,计算所得的广义位移时间响应曲线表明该叶片在近失速工况下会发生失速颤振,其表现形式为一阶弯曲模态发散且各阶模态之间不耦合。分析表明,流场不稳定和非定常效应是引起失速颤振的关键因素,同时折合频率的降低也会导致原本气动弹性稳定的叶片发生失速颤振。 相似文献