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《Astroparticle Physics》2009,32(1):10-41
We present a comprehensive report on the experimental details of the Antarctic Impulsive Transient Antenna (ANITA) long-duration balloon payload, including the design philosophy and realization, physics simulations, performance of the instrument during its first Antarctic flight completed in January of 2007, and expectations for the limiting neutrino detection sensitivity. 相似文献
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深空探测是对宇宙中地球以外的行星、卫星、小行星和彗星等星体或空间环境的探测活动.合理选择深空探测科学仪器,了解被测星体的物理及化学性质、地表地貌、动态特性以及有机物和水的存在,对人类了解地外水和生命信息、认识太阳系的起源和演化有着重要意义,是深空探测的重要任务.本文总结了深空探测的科学目标,介绍了近50年来典型深空探测任务中探测器所搭载的科学仪器及其特点,包括质谱仪、光谱仪、探地雷达和磁力计等,整理了其性能参数及面向的探测功能任务,最后讨论了深空探测科学仪器目前呈现出的小型化、低功耗、更强的环境适应能力和多仪器联合使用的发展趋势. 相似文献
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We present characterizations of the dynamic turbulence in the lower stratosphere measured by a new balloon-based system designed for detecting finer scale dynamic turbulence. The balloon-based system included a constant temperature anemometer(CTA) operating at a sampling rate of 2 k Hz at an ascent speed of 5 m s-1(corresponding to a vertical resolution of 2.5 mm), an industrial personal computer, batteries, sensors for ambient temperature and humidity, an A/D converter, and others. The system was successfully launched to 24 km altitude over Bayannur City, Inner Mongolia Province. Results show the spatial intermittence of the turbulence layers, with clear boundaries between turbulent and nonturbulent regions. This is the first time that the dynamic turbulence spectrum down to the viscous sub-range has been obtained throughout the lower stratosphere over China. With that, the energy dissipation rates of dynamic turbulence could be calculated with high precision. The profile of the dissipation rates varied from 7.37 × 10-7 to 4.23 W kg-1 and increased with altitude in the stratosphere. 相似文献
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提出一种基于连接载荷相似度的蠕虫检测方法 ,利用汉明距离计算载荷相似度检测未知蠕虫。与最长公共子串算法相比,这种方法更能减少计算资源消耗。并在此基础上,提出结合粗粒度异常检测和细粒度行为分析的检测系统。进一步排查非蠕虫流量,锁定蠕虫报文组,减少相似度的计算量。实验证明,这种方法能够检测出未知蠕虫。 相似文献
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内编队系统通过构造内卫星纯引力轨道完成高精度重力场测量,实现了不依赖于加速度计的重力卫星实施新途径.针对内编队系统轨道参数和载荷指标设计任务,从定性的角度分析了轨道高度、轨道倾角、偏心率等轨道参数的选择原则,以及外卫星定轨精度、内外卫星相对状态测量精度、内卫星非引力干扰抑制精度、系统采样率等载荷指标对内编队重力场测量性能的影响,并建立了这些参数之间的匹配关系.为获取内编队系统轨道参数和载荷指标的定量设计结果,给出了内编队重力场测量数据模拟和反演计算方法.结合轨道参数和载荷指标对重力场测量性能的影响及其匹配关系,提出了由解析推导和数值计算相结合的方法,获取重力场最高反演阶数、大地水准面精度、重力异常精度等重力场测量性能与轨道参数、载荷指标之间的解析关系,并给出了该解析关系的具体数学形式.与解析法、半解析法相比,该公式由解析推导和大量数值计算得到,因而考虑的影响因素更加全面,计算结果更加合理,可用于快速准确设计内编队系统轨道参数和载荷指标. 相似文献
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Convective storms and lightning are among the most important weather phenomena that are challenging to forecast. In this study, a novel multi-task learning(MTL) encoder-decoder U-net neural network was developed to forecast convective storms and lightning with lead times for up to 90 min, using GOES-16 geostationary satellite infrared brightness temperatures(IRBTs), lightning flashes from Geostationary Lightning Mapper(GLM), and vertically integrated liquid(VIL)from Next Generation Weather Radar... 相似文献
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使用机器学习进行遥感影像标注的一个重要前提是有足够的训练样本,而样本的标注是非常耗时的。本文采用了域适应的方法来解决遥感影像场景分类中小样本量的无监督学习问题,提出了结合对抗网络与辅助任务的遥感影像域适应方法。首先建立了基于深度卷积神经网络的遥感影像分类框架;其次,为了学习到域不变特征,在标签分类器的基础上增加域分类器,并使域损失函数在其反射传播时的梯度与标签损失的梯度相反,从而保证域分类器不能区分样本来自于哪个域;最后引入了辅助分类任务,扩充了样本的同时使网络更具泛化能力。试验结果表明,本文方法优于主流的无监督域适应方法,在小样本遥感影像无监督分类中得到了较好的效果。 相似文献
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A preliminary commission error analysis whereby orbit perturbation theory and other techniques are used to assess and predict the recovery of the Earths gravity field from the challenging microsatellite payload (CHAMP) mission is developed and implemented. With CHAMP launched in July 2000, accumulated evidence is now available to quantify the errors in the recovery procedure including the orbital precision from GPS, attitude errors, accelerometer noise and thruster mismatch/misalignment. For the latter, numerical integrations using a variable length single-step Runge–Kutta integrator and a fixed length multi-step method are compared to assess the error associated with assuming that the thruster misalignment can be spread uniformly across a step interval. Error degree variances from simulated studies are compared to results from a recently released CHAMP-based gravity field, EIGEN-1S. It is seen that the orbital positioning, as derived from the onboard GPS receiver, is critical, with accelerometer noise contributing at a lower level. Attitude error, at currently quoted accuracy, is not significant as an error source.
AcknowledgementsThe authors would like to thank the UK Natural Environment Research Council (Grant No. NER/A/0000/00612) for financing this study and GFZ for supplying the data and technical support. 相似文献