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基于三维曲面Spline模型研究中国不同地区的磁场分布
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作者 冯彦 黄娅 +2 位作者 李翊君 张晋源 刘爽 《Applied Geophysics》 SCIE CSCD 2024年第1期31-40,203,共11页
利用地面台站以及子午工程测点,CHAMP卫星实测数据,建立了中国地区主磁场的三维曲面Spline(3DSS)模型。基于该模型进行了我国的高原地区(青藏高原28°N-38°N,78°E-102°E)、平原地区(长江中下游平原27°N-34°... 利用地面台站以及子午工程测点,CHAMP卫星实测数据,建立了中国地区主磁场的三维曲面Spline(3DSS)模型。基于该模型进行了我国的高原地区(青藏高原28°N-38°N,78°E-102°E)、平原地区(长江中下游平原27°N-34°N,111°E-122°E)以及海洋地区(东海和南海部分区域16°N-30°N,123°E-136°E)的磁场模拟。分别基于高原及平原的实测数据建立了各自的3DSS模型。另外分别建立了对应的二维Taylor(2DTY)、三维Taylor多项式(3DTY)模型以比较验证。建模时考虑了所有测点的场源移除、地面及卫星数据间的数据真空、边界效应等问题。为了考察模型相对于实测值的模拟精度,对三个地区分别选取若干个测点不参与建模,将所建模型分别模拟这些测点,并计算残差、变化率及均方根偏差(RMSE)。结果显示无论是全国3DSS模型还是小区域3DSS模型,其变化率除了Y分量略大,其余分量都在1%以内,模拟精度均要好于2DTY和3DTY模型。小区域(高原及平原)3DSS模型能较好反映区域磁场分布。模型对高原的拟合最好,平原次之,海洋地区最差,说明3DSS模型不需要太多的测点即可完成建模,但建模精度依赖于测点的数量及分布。 展开更多
关键词 地磁场 三维模型 曲面spline 子午工程 CHAMP卫星 CM4
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B-Spline曲线聚风装置直线翼垂直轴风力机启动性能数值模拟
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作者 李岩 马云飞 +2 位作者 佟国强 杨胜兵 肖振军 《排灌机械工程学报》 CSCD 北大核心 2024年第3期265-272,共8页
为了提升直线翼垂直轴风力机的启动性能,基于B-Spline曲线生成方法,提出一种具有流线型轮廓的聚风装置,将其分别安装在风轮顶端和底端,用以提升风轮附近的来流风速,使风轮汲取更多风能,达到更易启动的特点.选取聚风装置的5个结构参数进... 为了提升直线翼垂直轴风力机的启动性能,基于B-Spline曲线生成方法,提出一种具有流线型轮廓的聚风装置,将其分别安装在风轮顶端和底端,用以提升风轮附近的来流风速,使风轮汲取更多风能,达到更易启动的特点.选取聚风装置的5个结构参数进行设计:聚风装置与风轮间隙距离ΔL、底圆半径R_(1)、顶圆半径R_(2)、入口角度α_(1)和出口角度α_(2).设计方法采用二次旋转正交组合筛选最优模型,通过三维数值模拟研究聚风装置参数对直线翼垂直轴风力机启动性能的影响,获得了最佳外形参数组合.此外,对有无加装聚风装置的直线翼垂直轴风力机进行了静态三维数值模拟.结果表明,通过添加具有外凸流线型轮廓的聚风装置,直线翼垂直轴风力机的启动性能有显著提升.在风速较低的情况下,性能改善更加明显.聚风装置可使直线翼垂直轴风力机的平均启动力矩系数最大增加38.8%,峰值平均启动力矩系数最大可增加31.2%. 展开更多
关键词 垂直轴风力机 聚风装置 B-spline曲线 启动性能 数值模拟
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基于Spline算法经编间隔织物的仿真建模
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作者 王文 邓中民 +1 位作者 李娟 柯薇 《针织工业》 北大核心 2024年第2期17-20,共4页
现阶段大多建模方法得到的模型保形性差,且缺少光照处理。文章提出一种基于Spline插值算法的建模方法,该方法保证曲线经过所有控制点,在三维空间上建立与实际织物基本相同的空间曲线,解决了以往所得模型保形性差的问题,并且通过VC++以及... 现阶段大多建模方法得到的模型保形性差,且缺少光照处理。文章提出一种基于Spline插值算法的建模方法,该方法保证曲线经过所有控制点,在三维空间上建立与实际织物基本相同的空间曲线,解决了以往所得模型保形性差的问题,并且通过VC++以及OpenGL开发工具,可以加上环境光照渲染、纹理处理等,使仿真模型更为写实,得到的仿真模型可以节省人力和物力及时间,能够在短时间内为设计人员提供更为准确的设计思路和方案。 展开更多
关键词 经编间隔织物 spline算法 OPENGL 仿真建模 保形性
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基于MARS的岩石抗拉强度预测模型
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作者 徐国权 王鑫瑀 《长江科学院院报》 CSCD 北大核心 2024年第2期135-141,共7页
将无损检测技术与机器学习相结合,通过建立预测模型来快速确定岩石抗拉强度已经成为热门研究方向之一。为了建立预测模型,提出一种基于多元自适应回归样条(MARS)的数据驱动建模技术,用于岩石抗拉强度预测。共收集了80组试验数据,包括施... 将无损检测技术与机器学习相结合,通过建立预测模型来快速确定岩石抗拉强度已经成为热门研究方向之一。为了建立预测模型,提出一种基于多元自适应回归样条(MARS)的数据驱动建模技术,用于岩石抗拉强度预测。共收集了80组试验数据,包括施密特回弹数、干密度、点荷载强度指数以及巴西抗拉强度。所有数据被随机分为2个部分,其中70%的数据用于训练模型,剩余30%的数据用于测试模型性能。同时开发了人工神经网络、支持向量机和决策树3种数据驱动模型。选择了4种常用的模型性能评价指标,分别为均方根误差、平均绝对误差、相关系数和决定系数,以此来对所开发模型的预测性能进行比较。结果表明:所开发的智能模型均能够提供较高的预测精度,其中MARS模型性能优于其他3种模型,支持向量机和人工神经网络模型次之,决策树模型相对较差。值得一提的是,MARS模型能够通过方差分析来评估每个变量的相对重要性。研究成果有助于快速确定岩石抗拉强度。 展开更多
关键词 岩石力学 抗拉强度 多元自适应回归样条(mars) 机器学习 预测模型
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Snow and regolith albedo variations using CRISM data at McMurdo crater,Mars
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作者 Sehajpal Singh Deepak Singh 《Earth and Planetary Physics》 EI CAS CSCD 2024年第2期338-355,共18页
The cryosphere component provides the most reliable and insightful indications of any planet’s climate dynamics.Using data from the Compact Reconnaissance Imaging Spectrometer for Mars(CRISM),we develop a novel appro... The cryosphere component provides the most reliable and insightful indications of any planet’s climate dynamics.Using data from the Compact Reconnaissance Imaging Spectrometer for Mars(CRISM),we develop a novel approach to determining the broadband Visible and Near Infrared(VNIR)albedo of the Martian surface.This study focuses on albedo changes in the McMurdo crater,part of Mars’s south polar layer deposits.We compare seasonal and interannual variations of the McMurdo surface albedo before,during,and after the Global Dust Storm(GDS)of Martian Year(MY)34.As the seasons progressed from spring to summer,the mean albedo in MY 32 and 34 plunged by over 40%,by about 35%in MY 33,and by slightly more than 30%in MY 35.Compared interannually,however,mean albedo values within both seasons(spring and summer)exhibited no significant differences in those same years.Notably,interannual albedo difference maps reveal albedo variation of more than±0.3 in certain regions of the crater.Considering only snow-covered pixels,interannual albedo differences suggest that Mars dust had a pervasive impact on Mars’s cryosphere.Variations in maximum and minimum albedo values as high as 0.5 were observed,depending upon differences in the dust levels in Martian snow/ice.The maximum and the minimum snow albedo values were lowest in MY 34,indicating the effect of the intense dust storm event that year.The average snow albedo decreased from 0.45 in MY 32 to 0.40 in MY 33 and to 0.33 in MY 34,and then rose back to 0.40 in MY 35.This trajectory suggests a temporary deposition of dust,partially reversed after the GDS by self-cleaning mechanisms(local aeolian process and CO_(2)sublimation/deposition cycle). 展开更多
关键词 mars Martian ice ALBEDO dust storm mars surface Martian climate
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MARS模型在渭河流域参考作物蒸散量计算中的适应性研究
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作者 葛杰 周晓平 +4 位作者 王晶 曹绮欣 曹钧恒 陈至立 冯家豪 《节水灌溉》 北大核心 2024年第2期17-24,共8页
为有效提高气象资料缺失时渭河流域参考作物蒸散量(ET_(0))计算精度,选取流域及附近20个气象站58 a(1960-2017年)逐日气象资料,基于不同气象要素组合,构建16种基于多元自适应回归样条(MARS)的ET_(0)计算模型,并将计算结果与Hargreaves-S... 为有效提高气象资料缺失时渭河流域参考作物蒸散量(ET_(0))计算精度,选取流域及附近20个气象站58 a(1960-2017年)逐日气象资料,基于不同气象要素组合,构建16种基于多元自适应回归样条(MARS)的ET_(0)计算模型,并将计算结果与Hargreaves-Samani、Makkink和Irmark-Allen模型进行对比,评价MARS模型在渭河流域的适应性及可移植性。结果表明:MARS模型能很好地甄别ET_(0)与各输入因子间的非线性关系,MARS2(T_(max)、T_(min)、R_(a))计算精度(平均MAE为0.225 mm/d,平均RMSE为0.327 mm/d,平均R2为0.897)能满足应用要求,模型精度随输入气象要素数量的增加而升高;输入因子中引入地球外辐射R_(a),可明显提高MARS模型精度;在输入因子相同时,MARS模型精度高于Hargreaves-Samani、Irmark-Allen和Makkink模型;MARS模型在渭河流域具有很强的泛化能力和可移植性。因此,气象资料缺失时基于MARS建立的ET_(0)计算模型可作为渭河流域ET_(0)计算的推荐模型。 展开更多
关键词 渭河流域 参考作物蒸散量 多元自适应回归样条 可移植性 ET_(0)模型 地球外辐射R_(a)
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用于超精密抛光机床的Spline+GLS定位误差补偿模型 被引量:1
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作者 潘海鸿 喻洪基 +2 位作者 陈旭红 陈琳 梁旭斌 《组合机床与自动化加工技术》 北大核心 2023年第5期156-159,163,共5页
针对三次样条插值定位误差补偿模型难达到超精密抛光机床大行程轴(1470 mm)的定位误差补偿精度要求问题,提出Spline+GLS定位误差补偿模型。首先,使用XL-80激光干涉仪测量超精密抛光机床直线电机轴的定位误差,建立三次样条插值定位误差... 针对三次样条插值定位误差补偿模型难达到超精密抛光机床大行程轴(1470 mm)的定位误差补偿精度要求问题,提出Spline+GLS定位误差补偿模型。首先,使用XL-80激光干涉仪测量超精密抛光机床直线电机轴的定位误差,建立三次样条插值定位误差补偿模型进行初补偿;然后,对补偿后的定位误差再次测量并建立最小二乘拟合定位误差补偿模型;最后,将两种定位误差补偿模型相连构成Spline+GLS定位误差补偿模型。在超精密抛光机床上进行补偿实验,结果表明,Spline+GLS定位误差补偿模型补偿后的最大定位偏差值较三次样条插值定位误差补偿模型下降约61.62%,且定位误差由86.12μm降低到0.5μm,满足超精密抛光机床的定位精度需求。 展开更多
关键词 超精密抛光机床 定位误差补偿 spline插值 GLS拟合
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能谱CT结合MARs技术对不同材质义齿伪影去除的临床价值 被引量:1
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作者 甘露 刘基 +4 位作者 袁晨 王玉恩 黎薛明 杨诗明 刘斌 《天津医药》 CAS 北大核心 2023年第6期642-647,共6页
目的研究能谱CT单能量成像及单能量+多伪影去除系统(MARs)去除义齿周围伪影的临床价值,并比较不同材质义齿对影像质量的影响。方法纳入100例有义齿植入的患者,义齿种类包括镍铬合金(30例)、烤瓷(30例)、胶托+不锈钢托(40例)。在相同CT... 目的研究能谱CT单能量成像及单能量+多伪影去除系统(MARs)去除义齿周围伪影的临床价值,并比较不同材质义齿对影像质量的影响。方法纳入100例有义齿植入的患者,义齿种类包括镍铬合金(30例)、烤瓷(30例)、胶托+不锈钢托(40例)。在相同CT扫描参数条件下进行能谱成像技术(GSI)扫描,获得混合能量(QC)影像、70~140 keV的单能量影像及单能量+MARs影像。在每例患者义齿伪影最严重层面和邻近无伪影的软组织区域划定2个感兴趣区(ROI):ROI1选取在同层无伪影的头夹肌处;ROI2选取在口腔中部舌部软组织明暗相间伪影区,ROI面积150~200 mm^(2),分别测量噪声(SD)、CT平均值,并计算伪影指数(AI),以SD和AI作为客观评价参数。由2名高年资放射科医师对各组影像质量进行主观评分。结果镍铬合金、烤瓷、胶托+不锈钢托3种材质义齿邻近组织的SD、AI随着管电压的增加而降低,在90 keV及以上时明显低于QC影像;单能量+MARs影像的SD和AI均明显低于同参数单能量影像;随着管电压的增加,口腔软组织的对比度明显降低,在110 keV+MARs时对比度最佳,主观评分最高。镍铬合金、烤瓷、胶托+不锈钢托3种材质义齿最佳成像参数比较,烤瓷的SD和AI最小。结论能谱扫描联合MARs技术能有效减少镍铬合金、烤瓷、胶托+不锈钢托的金属伪影,可作为去除口腔修复体伪影的有效方法。 展开更多
关键词 义齿 伪迹 mars技术 单能量技术 能谱成像
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Mountain permafrost distribution modeling using Multivariate Adaptive Regression Spline (MARS) in the Wenquan area over the Qinghai-Tibet Plateau 被引量:3
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作者 XiuMin Zhang ZhuoTong Nan +3 位作者 JiChun Wu ErJi Du Tong Wang YanHui You 《Research in Cold and Arid Regions》 2012年第5期361-370,共10页
In high mountainous areas, the development and distribution of alpine permafrost is greatly affected by macro- and mi- cro-topographic factors. The effects of latitude, altitude, slope, and aspect on the distribution ... In high mountainous areas, the development and distribution of alpine permafrost is greatly affected by macro- and mi- cro-topographic factors. The effects of latitude, altitude, slope, and aspect on the distribution of permafrost were studied to under- stand the dislribution patterns of permafrost in Wenquan on the Qinghai-Tibet Plateau. Cluster and correlation analysis were per- formed based on 30 m Global Digital Elevation Model (GDEM) data and field data obtained using geophysical exploration and borehole drilling methods. A Multivariate Adaptive Regression Spline model (MARS) was developed to simulate permafrost spa- tial distribution over the studied area. A validation was followed by comparing to 201 geophysical exploration sites, as well as by comparing to two other models, i.e., a binary logistic regression model and the Mean Annual Ground Temperature model (IVlAGT). The MARS model provides a better simulation than the other two models. Besides the control effect of elevation on permafrost distribution, the MARS model also takes into account the impact of direct solar radiation on permafrost distribution. 展开更多
关键词 permafrost distribution model Multivariate Adaptive Regression splines Qinghai-Tibet Plateau PERMAFROST
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基于二维B-splines方法研究强磁场中类氢离子He+的低能能级
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作者 刘凤丽 《黑龙江大学自然科学学报》 2023年第5期596-604,共9页
采用改进的二维B-spline方法在柱坐标系下研究了强磁场下类氢离子He^(+)的结构和电子空间几率密度,计算包含三种对称性0^(+)、0^(-)和(^(-)1)^(+)共10个本征态1 0^(+)、2 0^(+)、ν 0^(-)(ν=1~4)和ν(-1)^(+)(ν=1~4)的能级,选定磁感... 采用改进的二维B-spline方法在柱坐标系下研究了强磁场下类氢离子He^(+)的结构和电子空间几率密度,计算包含三种对称性0^(+)、0^(-)和(^(-)1)^(+)共10个本征态1 0^(+)、2 0^(+)、ν 0^(-)(ν=1~4)和ν(-1)^(+)(ν=1~4)的能级,选定磁感应强度分别为0、0.001、0.003、0.005、0.007、0.010、0.030、0.050、0.070、0.100、0.200、0.300、0.500、0.700和1.000 a.u.。计算结果表明,类氢离子He^(+)的能级在强磁场中发生劈裂,简并度消除,得到了各个能级随磁感应强度变化规律,并且发现随着磁感应强度的增加能级高低会改变,甚至会发生能级翻转现象;定量地研究了类氢离子He^(+)的基态1 0^(+)和激发态3 0^(-)几率密度分布随磁感应强度的变化规律,并与氢原子进行比较。本研究部分计算结果与他人研究结果十分吻合,有助于进一步理解其他复杂原子的电子运动行为。 展开更多
关键词 B-spline方法 类氢离子He+ 强磁场 能级
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基于Mars2000的船舶中剖面通用快速优化方法
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作者 汪俊泽 王元 +2 位作者 张攀 吴嘉蒙 程远胜 《中国舰船研究》 CSCD 北大核心 2023年第5期133-140,共8页
[目的]船舶中剖面优化具有设计变量多、约束条件复杂的特点。相关研究多采用智能优化算法直接嵌套规范校核软件(如Mars2000)的优化方法,计算量较大。为此,提出基于敏度排序的中剖面快速优化方法。[方法]首先计算各个约束特征量关于各设... [目的]船舶中剖面优化具有设计变量多、约束条件复杂的特点。相关研究多采用智能优化算法直接嵌套规范校核软件(如Mars2000)的优化方法,计算量较大。为此,提出基于敏度排序的中剖面快速优化方法。[方法]首先计算各个约束特征量关于各设计变量的敏度,根据敏度信息得到各特征量不满足约束时的设计变量调整次序,并判断各特征量是否只与局部构件相关。优化迭代时,根据当前方案的约束不满足情况,结合敏度信息做变量调整,并进行周期性的敏度更新。最后引入基于坐标轮换法的小范围调整方法进一步提升优化效果。[结果]某油船中剖面算例优化结果表明,所提方法可实现结构减重5.195%。[结论]与直接嵌套Mars2000的智能优化算法相比,本方法在优化效果相当的情况下,计算量仅为前者的5.58%左右,成本优势明显。 展开更多
关键词 中剖面 mars2000软件 船舶规范 优化
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Determining the moment of inertia of triaxial Mars with updated global gravity models 被引量:2
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作者 ChangYi Xu Yan Jiang 《Earth and Planetary Physics》 CAS CSCD 2023年第6期615-619,共5页
The principal moments of inertia(PMIs)with the principal axes are usually taken as the dynamic figure parameters of Mars;they can be deduced from satellite-observed degree-two gravitational potentials in recent global... The principal moments of inertia(PMIs)with the principal axes are usually taken as the dynamic figure parameters of Mars;they can be deduced from satellite-observed degree-two gravitational potentials in recent global gravity models and from the dynamic ellipticities resulting from precession observations.These PMIs are natural and significant for the geodetic,geophysical,and geodynamic problems of Mars,which are functions of internal density distributions.In this study,a closed and concise formula for determining the PMIs of the entire planet and its core was developed based on the second invariants of gravity and a multipole expansion.We deduced the polar oblateness J^(2)and the equatorial ellipticity J_(22)of Mars to be 1.9566×10^(−3)and 6.3106×10^(−5),respectively.The preferred principal moments of inertia of Mars are A=2.66589×1036 kg·m^(2),B=2.66775×10^(36)kg·m^(2),and C=2.68125×10^(36)kg·m^(2).These values indicate that Mar is slightly triaxial.The equatorial principal moment of inertia of the Martian core is 1.46008×10^(35)kg·m^(2),accounting for~5.47%of the planet’s PMI;this result is critical for investigating the density and size of the core of Mars,and the planet’s free core nutation. 展开更多
关键词 mars principal moment of inertia dynamic ellipticity Chandler wobble core density and size
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The Mars orbiter magnetometer of Tianwen-1:in-flight performance and first science results 被引量:1
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作者 YuMing Wang TieLong Zhang +17 位作者 GuoQiang Wang SuDong Xiao ZhuXuan Zou Long Cheng ZongHao Pan Kai Liu XinJun Hao YiRen Li ManMing Chen ZhouBin Zhang Wei Yan ZhenPeng Su ZhiYong Wu ChengLong Shen YuTian Chi MengJiao Xu JingNan Guo Yang Du 《Earth and Planetary Physics》 EI CSCD 2023年第2期216-228,共13页
The Mars Orbiter MAGnetometer(MOMAG)is a scientific instrument onboard the orbiter of China’s first mission for Mars—Tianwen-1.Since November 13,2021,it has been recording magnetic field data from the solar wind to ... The Mars Orbiter MAGnetometer(MOMAG)is a scientific instrument onboard the orbiter of China’s first mission for Mars—Tianwen-1.Since November 13,2021,it has been recording magnetic field data from the solar wind to the magnetic pile-up region surrounding Mars.Here we present its in-flight performance and first science results,based on its first one and one-half months’data.Comparing these early MOMAG observations to the magnetic field data in the solar wind from NASA’s Mars Atmosphere and Volatile EvolutioN(MAVEN)mission,we report that the MOMAG magnetic field data are at the same level in magnitude,and describe the same magnetic structures with similar variations in three components.We recognize 158 clear bow shock(BS)crossings in these MOMAG data;their locations match well statistically with the modeled average BS.We also identify and compare five pairs of datasets collected when Tianwen-1’s orbiter and the MAVEN probe made simultaneous BS crossings.These BS crossings confirm the global shape of modeled BS,as well as the south-north asymmetry of the Martian BS.Two cases presented in this paper suggest that the BS is probably more dynamic at flank than near the nose.So far,MOMAG performs well,and provides accurate magnetic field vectors.MOMAG is continuously scanning the magnetic field surrounding Mars.Data from MOMAG’s measurements complement data from MAVEN and will undoubt edly advance our understanding of the plasma environment of Mars. 展开更多
关键词 mars magnetic field Tianwen-1 magnetometer bow shock
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基于MARS和概率规划的离群值检测算法
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作者 王瑞豪 童英华 冯忠岭 《计算机工程与设计》 北大核心 2023年第9期2694-2699,共6页
为提高物联网数据质量,提出一种基于MARS模型和概率规划的多变量离群值检测方法。该方法能够将多个变量结合起来,通过一个模型检测离群值。创建一个多元自适应回归样条模型产生研究化的残差,将残差作为输入,采用概率规划方法,建立基于... 为提高物联网数据质量,提出一种基于MARS模型和概率规划的多变量离群值检测方法。该方法能够将多个变量结合起来,通过一个模型检测离群值。创建一个多元自适应回归样条模型产生研究化的残差,将残差作为输入,采用概率规划方法,建立基于全贝叶斯推理的一般单变量离群点检测模型。实验结果表明,概率规划模型能检测出更准确的离群点,该模型提供了具有可信区间的概率分布。 展开更多
关键词 物联网 数据质量 多元自适应回归模型 离群值 概率规划 多元离群点检测 贝叶斯
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Child Neurodevelopment on Mars
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作者 Tory L. Roberts 《Natural Science》 CAS 2023年第2期66-77,共12页
This review article aims to gather differences and similarities between planet Mars and planet Earth to determine the necessities for the proper growth and development of the neonatal brain. Factors such as Environmen... This review article aims to gather differences and similarities between planet Mars and planet Earth to determine the necessities for the proper growth and development of the neonatal brain. Factors such as Environmental, Nutritional, Social, Stress, and Education are juxtaposed to understand the difference between pediatric neurodevelopment on both planets. The variation between each factor was analyzed to determine how significant the impact is on neurodevelopment for children. The factors to be discussed were generated based on extensive research on what is most important for proper early neurodevelopment. The five factors are the main categories branched out into subcategories to delve into more detail regarding neurodevelopment. Factors may vary based on the location on each planet, but the best average was cultivated to create a fair evaluation of the differences. Although each factor influences a different part of the brain, each factor (Environmental, Nutritional, Social, Stress, and Education) is equally vital for development anatomy and physiology of the brain. 展开更多
关键词 NEURODEVELOPMENT mars PEDIATRIC NEUROSCIENCE NEONATAL mars Exploration mars Environment
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Observation 20-s periodic signals on Mars from InSight,Sols 800-1,000
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作者 HuiXing Bi DaoYuan Sun MingWei Dai 《Earth and Planetary Physics》 EI CSCD 2023年第2期193-215,共23页
Seismometers of the InSight probe(Interior Exploration using Seismic Investigation,Geodesy and Heat Transport)currently operating on Mars have recorded not only seismic events but also high-frequency non-seismic perio... Seismometers of the InSight probe(Interior Exploration using Seismic Investigation,Geodesy and Heat Transport)currently operating on Mars have recorded not only seismic events but also high-frequency non-seismic periodic signals that appear to have been induced by variations in the Martian environment and the hardware.Here,we report an observation of a long-period signal with a dominant period of~20 s from Martian solar days(Sol)800 to Sol 1,000.This 20-s signal is detected mostly at quiet nighttime—from22:00 to 04:00 LMST(Local Mean Solar Time)—at the InSight landing site.The measurement of the particle motion suggests that this linearly polarized signal focuses on the horizontal plane with an angle of~30°from the north.By examining the temporal variation of the signal’s amplitude and polarization angle and its times of occurrence in relation to the planet’s atmospheric data,we suggest that this20-s signal may be relevant to wind and temperature variations on Mars.Furthermore,we study the possible influence of this 20-s signal on the noise autocorrelation and find that the stacked autocorrelograms can be quite different when the 20-s signal is present. 展开更多
关键词 mars periodic signal particle motion AUTOCORRELATION
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Numerical Study on Low-Reynolds Compressible Flows around Mars Helicopter Rotor Blade Airfoil
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作者 Takuma Yamaguchi Masayuki Anyoji 《Journal of Flow Control, Measurement & Visualization》 CAS 2023年第2期30-48,共19页
High-speed rotor rotation under the low-density condition creates a special low-Reynolds compressible flow around the rotor blade airfoil where the compressibility effect on the laminar separated shear layer occurs. H... High-speed rotor rotation under the low-density condition creates a special low-Reynolds compressible flow around the rotor blade airfoil where the compressibility effect on the laminar separated shear layer occurs. However, the compressibility effect and shock wave generation associated with the increase in the Mach number (M) and the trend change due to their interference have not been clarified. The purpose is to clear the compressibility effect and its impact of shock wave generation on the flow field and aerodynamics. Therefore, we perform a two-dimensional unsteady calculation by Computational fluid dynamics (CFD) analysis using the CLF5605 airfoil used in the Mars helicopter Ingenuity, which succeeded in its first flight on Mars. The calculation conditions are set to the Reynolds number (Re) at 75% rotor span in hovering (Re = 15,400), and the Mach number was varied from incompressible (M = 0.2) to transonic (M = 1.2). The compressible fluid dynamics solver FaSTAR developed by the Japan aerospace exploration agency (JAXA) is used, and calculations are performed under multiple conditions in which the Mach number and angle of attack (α) are swept. The results show that a flow field is similar to that in the Earth’s atmosphere above M = 1.0, such as bow shock at the leading edge, whereas multiple λ-type shock waves are observed over the separated shear layer above α = 3° at M = 0.80. However, no significant difference is found in the C<sub>p</sub> distribution around the airfoil between M = 0.6 and M = 0.8. From the results, it is found that multiple λ-type shock waves have no significant effect on the airfoil surface pressure distribution, the separated shear layer effect is dominant in the surface pressure change and aerodynamic characteristics. 展开更多
关键词 CFD CLF5605 Rotor Blade Airfoil Compressibility Effect Low-Reynolds Number mars Helicopter Separation Bubble Shock Wave
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Analyzing Whether a Space Shuttle Can Withstand a Perpendicular Launch from Mars
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作者 Mayank Banerjee 《Natural Science》 2023年第10期257-262,共6页
In the near future, humans will go to Mars. During these interplanetary journeys, astronaut safety will be paramount. This study aims to determine whether the astronauts will be able to launch safely from Mars in a sp... In the near future, humans will go to Mars. During these interplanetary journeys, astronaut safety will be paramount. This study aims to determine whether the astronauts will be able to launch safely from Mars in a space shuttle taking off perpendicularly. This study used kinematics along with equations for calculating atmospheric density and total force on the spacecraft to evaluate these values for each atmospheric layer. Approximations were made for the spacecraft’s dimensions to find the cross-sectional front-view area of the spacecraft and the drag coefficient where verifiable data was unavailable. Although there is data for the dimensions of the spacecraft’s front view, there isn’t any on its area. The total force was found to be significantly lower than 3Gs which ensures a safe take-off for the astronauts and reduces manufacturing costs for assembling new rockets. 展开更多
关键词 Space Shuttle Spacecraft mars ROCKET Physics Atmosphere Drag Gravity ASTRONAUT Force THRUST Fuel
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Observations and interpretations of geomorphologic features in the Tianwen-1 landing area on Mars by using orbital imagery data
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作者 Hai Huang Xing Wang +10 位作者 Yuan Chen Qing Zhang FeiYue Zhao Xin Ren XingGuo Zeng Wei Yan WangLi Chen Bin Liu DaWei Liu LianBo Fu JianJun Liu 《Earth and Planetary Physics》 EI CSCD 2023年第3期331-346,共16页
China’s first Mars exploration mission,Tianwen-1,successfully landed in southern Utopia Planitia on Mars on May 15,2021.This work presents a detailed investigation of the geologic context of the landing area surface ... China’s first Mars exploration mission,Tianwen-1,successfully landed in southern Utopia Planitia on Mars on May 15,2021.This work presents a detailed investigation of the geologic context of the landing area surface for this mission based on orbital remotesensing data.We constructed a geomorphologic map for the Tianwen-1 landing area.Results of our detailed geomorphologic map show several major landforms within the landing area,including rampart craters,mesas,troughs,cones,and ridges.Analysis of materials on the landing area surface indicates that most of the landing area is covered by Martian dust.Transverse aeolian ridges are widely distributed within the landing area,indicating the surface contexts were(and still are)modified by regional winds.In addition,a crater counting analysis indicates the landing area has an absolute model age of~3.3 Ga and that a later resurfacing event occurred at~1.6 Ga.Finally,we outline four formational scenarios to test the formation mechanisms for the geomorphologic features on the landing area surface.The most likely interpretation to explain the existence of the observed surface features can be summarized as follows:A thermal influence may have played an important role in the formation of the surface geomorphologic features;thus,igneous-related processes may have occurred in the landing area.Water ice may also have been involved in the construction of the primordial surface configuration.Subsequent resurfacing events and aeolian processes buried and modified the primordial surface. 展开更多
关键词 mars Utopia Planitia Tianwen-1 geomorphologic features water ice heat source
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Ground calibration of the Mars orbiter magnetometer onboard Tianwen-1
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作者 ManMing Chen Kai Liu +3 位作者 XiaoWen Hu YiRen Li XinJun Hao ZongHao Pan 《Earth and Planetary Physics》 EI CSCD 2023年第3期371-377,共7页
Ground calibration experiments of the Mars orbiter magnetometer(MOMAG)onboard the orbiter of Tianwen-1 were performed to determine the sensitivity,misalignment angle,and offset of the sensors.The linearity of the appl... Ground calibration experiments of the Mars orbiter magnetometer(MOMAG)onboard the orbiter of Tianwen-1 were performed to determine the sensitivity,misalignment angle,and offset of the sensors.The linearity of the applied calibrated magnetic fields and the output from the sensors were confirmed to be better than 10^(-4),and the sensor axes were orthogonal to each other within 0.5 degrees.The temperature dependencies of the sensitivity and misalignment angle were examined,but no clear signatures of temperature dependencies could be seen.Sensor offset and the stability of sensor offset drift with a temperature change were also determined by the rotation method.The stability of the sensor offset drift was less than 0.01 nT/℃.The ground calibration of MOMAG determines all the calibration parameters of the sensors for accurate magnetic field measurements in orbit with the appropriate corrections. 展开更多
关键词 mars orbiter magnetometer Tianwen-1 ground calibration
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