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Prototype design of satellite payload for neutron spectrum acquisition
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作者 Xiao-Li Wang Shu-Cheng Shi +4 位作者 Chen-Yao Han Yi-Ming Ma Quan-Qi Shi Shuai Wang Jiao Feng 《Nuclear Science and Techniques》 2026年第4期5-18,共14页
In recent years,there have been fewer missions to detect neutrons in low Earth orbits(LEO),and the data obtained have been extremely limited.Studying the distribution of the neutron energy spectrum in LEO satellites t... In recent years,there have been fewer missions to detect neutrons in low Earth orbits(LEO),and the data obtained have been extremely limited.Studying the distribution of the neutron energy spectrum in LEO satellites through detection can help solve three major scientific problems:the source of particles in the inner radiation belt,information on solar-accelerated particles,and the proportion of neutrons from different sources in near-Earth space.The detection efficiency and accuracy of neutrons are affected by charged and primary particles in the environment and secondary neutrons produced by the spacecraft itself,which has been a hot research topic.The neutron spectrometer developed in this study adopts two combinations of 15 silicon detectors in terms of detector type and arrangement,which are used for neutron detection via the nuclear reaction method and recoil proton method,respectively,in which a 27μm-thick^(6)LiF conversion layer is used for thermal neutron detection up to 0.4 eV and a 300μm-thick high-density polyethylene conversion layer is used for fast-neutron detection up to 14 MeV and below.The design of the detector set can also remove the influence of primary charged particles and secondary neutrons in the detection environment to a certain extent,thereby improving the accuracy of neutron detection.In this study,the neutron spectrometer hardware,firmware,software design,and basic performance of the front-end readout chip SKIROC2A were tested.The readout circuit of each channel baseline ADC code was less than 17;thus,the channel consistency was good.The RMS noise of the channel baseline was only 7.1 mV and exhibited good stability.The maximum number of events that could be processed per second is 75.The overall power consumption was 3 W,the weight was 792 g,and the volume was less than 1 dm^(3).Furthermore,the neutron spectrometer was tested for principle and detection efficiency using various neutron sources,such as ^(241)Am-Be neutron source,2.5 MeV neutron beam,and 14 MeV neutron beam,and the experiments were analyzed with corresponding simulations.The experimental data and simulation results were in good agreement and met the design requirements.The intrinsic detection efficiency of the probes used in the neutron spectrometer was 1.05%for 14 MeV fast neutrons. 展开更多
关键词 Neutron spectrometer Satellite payload Prototype design GEANT4 SKIROC2A
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Study on correlation of thermal model to in-orbit data for infrared optical payloads on FY-3E/HIRAS-Ⅱ
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作者 LI Yu-Han YANG Bao-Yu +4 位作者 ZHANG Qiang GUO Zhi-Peng WU Yi-Nong TANG Xiao LI Shang-Ju 《红外与毫米波学报》 北大核心 2025年第3期394-405,共12页
The Infrared Hyperspectral Atmospheric SounderⅡ(HIRAS-Ⅱ)is the key equipment on FengYun-3E(FY-3E)satellite,which can realize vertical atmospheric detection,featuring hyper spectral,high sensitivity and high precisio... The Infrared Hyperspectral Atmospheric SounderⅡ(HIRAS-Ⅱ)is the key equipment on FengYun-3E(FY-3E)satellite,which can realize vertical atmospheric detection,featuring hyper spectral,high sensitivity and high precision.To ensure its accuracy of detection,it is necessary to correlate their thermal models to in-orbit da⁃ta.In this work,an investigation of intelligent correlation method named Intelligent Correlation Platform for Ther⁃mal Model(ICP-TM)was established,the advanced Kriging surrogate model and efficient adaptive region opti⁃mization algorithm were introduced.After the correlation with this method for FY-3E/HIRAS-Ⅱ,the results indi⁃cate that compared with the data in orbit,the error of the thermal model has decreased from 5 K to within±1 K in cold case(10℃).Then,the correlated model is validated in hot case(20℃),and the correlated model exhibits good universality.This correlation precision is also much superiors to the general ones like 3 K in other similar lit⁃erature.Furthermore,the process is finished in 8 days using ICP-TM,the efficiency is much better than 3 months based on manual.The results show that the proposed approach significantly enhances the accuracy and efficiency of thermal model,this contributes to the precise thermal control of subsequent infrared optical payloads. 展开更多
关键词 thermal model intelligent correlation method surrogate model infrared optical payload FY-3E
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Aerodynamic mechanism and aeroacoustic analysis of rocket sled with winged payload
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作者 Haojun LI Wenjie WANG +1 位作者 Xinyu MA Xu ZHAO 《Chinese Journal of Aeronautics》 2025年第9期114-125,共12页
The rocket sled system is not only a high-speed dynamic ground test system,but also one of the future aerospace horizontal launch schemes.The winged load,as a common type of payload,has greater vibration and noise int... The rocket sled system is not only a high-speed dynamic ground test system,but also one of the future aerospace horizontal launch schemes.The winged load,as a common type of payload,has greater vibration and noise intensity than the wingless load.Due to the severe aerodynamic instability prior to separation,the head-up or head-down phenomena are more evident and the test accuracy significantly decreases.The high-precision computer fluid dynamics and aeroacoustic analysis are employed to explore the multifield coupling mechanism of a rocket sled with the winged payload in the wide speed range(Ma=0.5–2).The results show that as the incoming velocity increases,the cone angle of the shock wave of the rocket sled decreases,the shock pressure increases quickly,and the vortex between the slippers splits and gradually shrinks in size.The velocity of the rocket sled exerts little influence on the modal resonance frequency.The wing has a significant impact on aerodynamic noise,and as the sound pressure level rises,the propagation direction gradually shifts towards the rear and upper regions of the wing. 展开更多
关键词 Aeroacoustic analysis Modal analysis Multifield coupling mechanism Rocket sled Winged payload
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基于大语言模型的SQL注入漏洞检测载荷生成方法
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作者 顾兆军 李丽 隋翯 《信息网络安全》 北大核心 2026年第2期274-290,共17页
针对现有SQL注入漏洞检测方法存在鲁棒性不足以及测试用例缺乏针对性等问题,文章提出一种基于大语言模型的SQL注入漏洞检测载荷生成方法。该方法通过生成针对性的检测载荷实现SQL注入漏洞检测,借助提示工程与DeepSeek-V3模型自动提取和... 针对现有SQL注入漏洞检测方法存在鲁棒性不足以及测试用例缺乏针对性等问题,文章提出一种基于大语言模型的SQL注入漏洞检测载荷生成方法。该方法通过生成针对性的检测载荷实现SQL注入漏洞检测,借助提示工程与DeepSeek-V3模型自动提取和统一构建漏洞特征;利用贡献度对漏洞特征进行分析和选择,构建模型的核心输入;通过将关键特征组织成思维链的形式促进多维度漏洞表征融合,并采用低秩适配技术对Qwen模型进行领域自适应监督微调。实验在多个公开漏洞靶场中验证Qwen模型与SqliGPT、GPT-2-web和SQLMap等模型的性能差异和生成质量,并深入分析DeepSeek-V3模型在复杂SQL注入漏洞数据中的特征提取能力。实验结果表明,Qwen模型的平均检测准确率达到75%以上,比SqliGPT、GPT-2-web和SQLMap模型分别提升49.18%、59.64%和15.19%,且载荷生成质量显著优于现有模型,证明了基于大语言模型生成检测载荷,实现SQL注入漏洞检测方法的有效性与优越性。 展开更多
关键词 大语言模型 SQL注入漏洞 代码生成 检测载荷
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红外感知的前沿热点:从深空探测极限到数字地球新范式
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作者 刘银年 《红外》 2026年第1期1-16,共16页
本文介绍了红外感知技术在“向上看”的深空探测与“向下看”的对地观测两大领域的发展脉络和前沿挑战。在深空探测方面,以詹姆斯·韦布空间望远镜(James Webb Space Telescope, JWST)为代表,该技术正通过超大口径、甚长波段和超低... 本文介绍了红外感知技术在“向上看”的深空探测与“向下看”的对地观测两大领域的发展脉络和前沿挑战。在深空探测方面,以詹姆斯·韦布空间望远镜(James Webb Space Telescope, JWST)为代表,该技术正通过超大口径、甚长波段和超低温制冷等手段,不断逼近观测的物理极限,并致力于揭示宇宙早期的历史奥秘。阐述了对地观测领域不同时期搭载于各类卫星的红外探测载荷的主要发展过程及其代表性和特色。红外对地观测技术从过去宽幅下的低空间分辨率和少量波段,向着空谱大范围下的时-空-谱-辐分辨率提升迈进。大口径低背景光学、长波长高灵敏度探测器、片上智能感知、大数据孪生系统等新型技术,以及通导遥一体的“即时遥感”和商业航天的大规模发展,将助力构建“红外数字地球”底座,增强人类对地球多圈层异常事件以及各种复杂循环过程演变的实时认知和精准预测,推动红外对地观测技术走向大众化应用。 展开更多
关键词 红外前沿 深空探测 对地观测 卫星载荷 数字地球
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基于文献计量学的中国探月工程国际科研影响力评估
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作者 张腾飞 徐琳 +4 位作者 杨蔚 王燕海 韩娟娟 林杨挺 李献华 《空间科学学报》 北大核心 2026年第1期1-21,共21页
基于Web of Science核心合集数据库,采用文献计量学方法对中国探月工程(2003-2024)的科研产出进行系统分析.通过量化评估1023篇SCI论文的时空分布特征、国际合作态势及学术影响力,揭示了中国探月工程对全球月球科学研究的贡献.研究表明... 基于Web of Science核心合集数据库,采用文献计量学方法对中国探月工程(2003-2024)的科研产出进行系统分析.通过量化评估1023篇SCI论文的时空分布特征、国际合作态势及学术影响力,揭示了中国探月工程对全球月球科学研究的贡献.研究表明,中国探月工程的实施使中国月球科学领域发文量占比提升至32.6%(2024年),工程产出论文的CNCI值(1.03)超越全球均值;科研突破集中于嫦娥四号(月球背面着陆巡视探测)与嫦娥五号(月球样品分析)任务,产出181篇高影响力论文;国际引用情况中,非中国机构占比显著增长,显示工程成果获得广泛国际认可.研究成果为评估中国深空探测计划的科学效益提供了定量依据. 展开更多
关键词 文献计量 月球科学 中国探月工程(嫦娥工程) 月球样品 有效载荷(科学载荷) 国际影响力
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无人机多模态超宽谱认知仪研究
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作者 施云鹤 张小飞 吴启晖 《数据采集与处理》 北大核心 2026年第1期28-52,共25页
本文设计了一种无人机(Unmanned aerial vehicle,UAV)多模态超宽谱认知仪,通过深度融合可见光、红外、合成孔径雷达(Synthetic aperture radar,SAR)及无线频谱等多模态传感器构建智能遥感系统,旨在攻克传统无人机遥感的根本性瓶颈:续航... 本文设计了一种无人机(Unmanned aerial vehicle,UAV)多模态超宽谱认知仪,通过深度融合可见光、红外、合成孔径雷达(Synthetic aperture radar,SAR)及无线频谱等多模态传感器构建智能遥感系统,旨在攻克传统无人机遥感的根本性瓶颈:续航时间短严重制约探测范围、有效载荷不足限制多模态感知能力、机载算力薄弱导致实时处理延迟、通信容量有限阻碍高保真态势评估。本文设计方案针对续航挑战,采用活塞发动机与锂电池协同的混合能源构型,结合垂直起降(Vertical take-off and landing,VTOL)飞翼布局,显著提升航时效能;为应对载荷限制,开发复眼多目相机实现大视场高分辨率成像,集成W波段轻小型SAR突破亚毫米级振动补偿技术,支撑空-时-频多维度协同感知;为化解实时处理困境,基于时空配准框架与轻量化深度学习模型,构建数据层-特征层-语义层多层次融合机制,将低可观测目标检测精度提升至90%以上;针对通信瓶颈,创新生成式编码技术结合知识图谱驱动的态势重建,通过无参考质量评估模型量化语义保真度,实现超400倍压缩下的高保真三维态势生成。该仪器在国防侦察领域成功实现复杂电磁环境中隐蔽目标实时追踪,在应急救援中完成洪涝灾害监测与三维重建等关键任务,验证了多模态超宽谱认知在复杂场景的实用价值。 展开更多
关键词 无人机 混合能源 多模态载荷集成 多模态融合 质量评估
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一种仪器设备高集密度的载荷舱布局优化方法
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作者 郭琳 赵佩麟 单颖蕾 《航天器工程》 北大核心 2026年第1期63-69,共7页
针对大型航天器仪器设备高集密度的载荷舱布局问题,提出一种两阶段布局优化算法,使用分段策略,聚焦主要技术约束,将一个高维多约束的优化问题分解为两阶段串联布局优化问题来解决。首先,对设备组件热管分配关系进行整数规划,分别加入热... 针对大型航天器仪器设备高集密度的载荷舱布局问题,提出一种两阶段布局优化算法,使用分段策略,聚焦主要技术约束,将一个高维多约束的优化问题分解为两阶段串联布局优化问题来解决。首先,对设备组件热管分配关系进行整数规划,分别加入热管多能承载的最大热功耗约束、纵向布局尺寸约束、组件布局的特殊约束和组件质心约束,确定最终的设备组件热管分配关系。然后通过根据分配关系进行详细布局优化问题建模,缩小组件的移动范围,优化质心位置,获得设计结果,输出设备位置确定布局设计方案。通过一个包含119台设备的载荷舱布局设计案例,获得了较好的载荷舱布局设计方案,验证了该方法处理大规模复杂设计问题时的能力,特别是质心约束不特别严苛的情况下,可以有效地生产布局方案,显示出良好的工程应用前景。 展开更多
关键词 航天器 载荷舱布局 多目标优化 散热 质心
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基于报文语义融合的加密恶意流量检测
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作者 何文林 邱建霖 +3 位作者 叶丹莲 吴贞东 黄达文 张倩 《四川师范大学学报(自然科学版)》 2026年第2期246-255,共10页
现有加密恶意流量检测模型通过学习流量特征内在联系来提高检测性能,主要面临报文时空特征维度较高、流量多维特征学习不足等挑战.面对上述挑战,提出一种基于报文语义融合的加密恶意流量检测模型(MSF).首先,将加密流量数据包拆分成多个... 现有加密恶意流量检测模型通过学习流量特征内在联系来提高检测性能,主要面临报文时空特征维度较高、流量多维特征学习不足等挑战.面对上述挑战,提出一种基于报文语义融合的加密恶意流量检测模型(MSF).首先,将加密流量数据包拆分成多个会话,提取关键行为特征并构建表征向量;其次,采用多头注意力机制学习流量特征权重,结合BiLSTM网络深度挖掘流量交互行为,捕获报文负载深层语义.同时,利用离散傅里叶变换压缩高维时空特征,并借助LSTM学习时空语义,实现高效特征降维与语义提取.最后,通过融合报文负载与时空语义,显著增强特征向量的表达能力,提升模型检测准确率.在DataCon 2020和Stratosphere两个公开数据集上进行对比实验,通过对比基线模型,MSF模型在DataCon 2020数据集上,精确率最高提高了16.7%,在Stratosphere数据集上的检测精确率表现最优,验证了模型的有效性. 展开更多
关键词 加密恶意流量检测 报文负载语义 报文时空语义 语义融合
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基于PayLoad特征的P2P IPTV应用识别 被引量:2
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作者 樊鹏翼 王晖 徐周李 《微计算机信息》 2009年第12期49-50,62,共3页
近年来,基于P2P流媒体技术的网络电视已经成为网络舆论传播的重要手段之一,而P2P技术的无中心和自组织特性将大大增加对网络电视服务进行识别和监管的难度。本文首先通过对不同IPTV的payload数据分析,发现P2PIPTV系统通信过程中均存在... 近年来,基于P2P流媒体技术的网络电视已经成为网络舆论传播的重要手段之一,而P2P技术的无中心和自组织特性将大大增加对网络电视服务进行识别和监管的难度。本文首先通过对不同IPTV的payload数据分析,发现P2PIPTV系统通信过程中均存在访问地址特征、协议定义特征以及数据传输特征,然后提出了基于以上三种特征相结合的识别方法,并设计实现了实时识别系统,最后利用统计实验验证了系统的识别精度并对实验进行了分析。 展开更多
关键词 P2P流媒体 payload特征 流量识别
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基于流量和payload双重特征识别P2P流量
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作者 卢慧 李华 吴承勇 《中国教育网络》 2015年第7期79-80,共2页
随着Internet的飞速发展,网络应用层出不穷,除了传统的Web、FTP、Email外,出现了高清晰音视频传输和交流,电影、游戏、音乐下载等数据流量剧增的各种P2P应用。P2P共享软件以其独特的优势为用户提供更为快捷的资源共享方式,因此受到广大... 随着Internet的飞速发展,网络应用层出不穷,除了传统的Web、FTP、Email外,出现了高清晰音视频传输和交流,电影、游戏、音乐下载等数据流量剧增的各种P2P应用。P2P共享软件以其独特的优势为用户提供更为快捷的资源共享方式,因此受到广大用户的喜爱,但随着其用户数量的急剧增加,也给校园网络带宽带来了巨大的压力,并对校园网络流量产生了根本影响。 展开更多
关键词 payload P2P流 下行流 网络出口 音视频传输 特征识别 音乐下载 网络带宽 特征匹配 MATCH
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具有精确质量估计的5-DOF塔机定位防摆控制
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作者 刘灿 侯传晶 李轾 《自动化技术与应用》 2026年第3期62-67,156,共7页
由于塔式起重机具有欠驱动、非线性、高耦合特性以及参数不确定性,导致其定位防摆控制成为一个难题。为了有效实现小车、悬臂和线缆的精确定位以及负载的摆动抑制,基于没有线性化处理的具有时变线缆长度的5-DOF塔机模型,提出了一种自适... 由于塔式起重机具有欠驱动、非线性、高耦合特性以及参数不确定性,导致其定位防摆控制成为一个难题。为了有效实现小车、悬臂和线缆的精确定位以及负载的摆动抑制,基于没有线性化处理的具有时变线缆长度的5-DOF塔机模型,提出了一种自适应积分滑模控制方案。首先,基于状态变量的误差值设计了一种积分滑模面,能够有效抑制负载摆动并且消除稳态误差,实现精确定位和摆动抑制。然后,设计了一种滑模趋近律,能够提高收敛速度并且有效抑制抖振问题。最后,通过设计自适应方案来抵消未知摩擦的影响以及精确估计不确定负载质量,消除垂直方向上的定位误差。通过严格的理论分析证明了闭环系统的稳定性。仿真结果验证了所提出方法具有良好的控制性能和鲁棒性。 展开更多
关键词 塔式起重机 滑模控制 自适应控制 负载质量估计 鲁棒性
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Real-time quality control of data from Sea-Wing underwater glider installed with Glider Payload CTD sensor 被引量:4
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作者 Zenghong Liu Jianping Xu Jiancheng Yu 《Acta Oceanologica Sinica》 SCIE CAS CSCD 2020年第3期130-140,共11页
Profiles observed by Sea-Wing underwater gliders are widely applied in scientific research. However, the quality control(QC) of these data has received little attention. The mismatch between the temperature probe and ... Profiles observed by Sea-Wing underwater gliders are widely applied in scientific research. However, the quality control(QC) of these data has received little attention. The mismatch between the temperature probe and conductivity cell response times generates erroneous salinities, especially across a strong thermocline. A sensor drift may occur owing to biofouling and biocide leakage into the conductivity cell when a glider has operated for several months. It is therefore critical to design a mature real-time QC procedure and develop a toolbox for the QC of Sea-Wing glider data. On the basis of temperature and salinity profiles observed by several Sea-Wing gliders each installed with a Sea-Bird Glider Payload CTD sensor, a real-time QC method including a thermal lag correction, Argo-equivalent real-time QC tests, and a simple post-processing procedure is proposed. The method can also be adopted for Petrel gliders. 展开更多
关键词 Sea-Wing underwater GLIDER GLIDER payload CTD SENSOR thermal lag correction quality-control tests
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In-flight performance analysis of the navigation augmentation payload on LEO communication satellite:a preliminary study on WT01 mission 被引量:5
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作者 Ziqian Wu Baoguo Yu +3 位作者 Chuanzhen Sheng Jingkui Zhang Song Xie Cailun Wu 《Geo-Spatial Information Science》 SCIE EI CSCD 2022年第1期88-103,共16页
With the development of the Low Earth Orbit(LEO)communication constellations,it has become a hot area of research to provide additional navigation augmentation services.Limited by volume,weight,power consumption,and r... With the development of the Low Earth Orbit(LEO)communication constellations,it has become a hot area of research to provide additional navigation augmentation services.Limited by volume,weight,power consumption,and running time,the in-flight performance of navigation augmentation payload remains to be investigated.In this paper,we analyze the data quality of on-board GNSS observation and evaluate the precision of short-arc dynamic Precise Orbit Determination(POD)performance based on the WangTong-01(WT01)mission.Furthermore,the downlink navigation measurement data of WT01 satellites are analyzed and compared with the GNSS observations.The results show that the average multipath errors of the WT01 on-board GPS L1,L2 and BeiDou Satellite Navigation System(BDS)B1,B2 code observation are 0.54,0.74,0.65,and 0.58 m,respectively.The short-arc dynamic POD three-dimensional(3D)overlapping accuracy is 7.1 cm.The average multipath errors of downlink navigation signal Z1 and Z2 are 0.81 and 0.80 m,respectively,which at the same order of magnitude as GNSS signals.The maximum Carrier-to-Noise Ratio(C/N0)value of WT01 downlink measurement data can reach 60 dB Hz,which is much stronger than GNSS and indicates the navigation signals of LEO satellites can meet the basic requirement of navigation augmentation. 展开更多
关键词 Navigation payload in-flight performance augmentation communication satellites LEO
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Preliminary Scientific Results of Chang'E-1 Lunar Orbiter:Based on Payloads Detection Data in the First Phase 被引量:24
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作者 OUYANG Ziyuan JIANG Jingshan LI Chunlai SUN Huixian ZOU Yongliao LIU Jianzhong LIU Jianjun ZHAO Baochang REN Xin YANG Jianfeng ZHANG Wenxi WANG Jianyu MOU Lingli CHANG Jin ZHANG Liyan WANG Huanyu LI Yongquan ZHANG Xiaohui ZHENG Yongchun WANG Shijin BIAN Wei 《空间科学学报》 CAS CSCD 北大核心 2008年第5期361-369,共9页
Chang'E-1 lunar Orbiter was launched by Long March 3A rocket from Xichang Satel-lite Launch Center at 18:05BT(Beijing Time) Oct.24,2007.It is the first step of its ambitious three-stage moon program,a new mileston... Chang'E-1 lunar Orbiter was launched by Long March 3A rocket from Xichang Satel-lite Launch Center at 18:05BT(Beijing Time) Oct.24,2007.It is the first step of its ambitious three-stage moon program,a new milestone in the Chinese space exploration history.The primary science objectives of Chang'E-1 lunar orbiter are to obtain three-Dimension(3D) stereo images of the lunar surface,to analyze the distribution and abundance of elements on the surface,to investigate the thickness of lunar soil,evaluate helium-3 resources and other characteristics,and to detect the space environment around the moon.To achieve the above four mission objectives,eight sets of scientific instruments are chosen as the payloads of the lunar orbiter,including a CCD stereo camera(CCD),a Sagnac-based interferometer spectrometer(ⅡM),a Laser Altimeter(LAM),a Microwave Radiometer(MRM),a Gamma-Ray Spectrometer(GRS),an X-ray spectrometer(XRS),a High-Energy Particle Detector(HPD),and two Solar Wind Ion Detectors(SWID).The detected data of the payloads show that all payloads work well.This paper introduces the status of payloads in the first phase and preliminary scientific results. 展开更多
关键词 嫦娥一号 空间研究 中国 宇航员
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The payloads of planetary physics research onboard China’s First Mars Mission (Tianwen-1) 被引量:9
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作者 WeiXing Wan Chi Wang +2 位作者 ChunLai Li Yong Wei JianJun Liu 《Earth and Planetary Physics》 CSCD 2020年第4期331-332,共2页
Mars is not only our nearby but also the most Earth-like planetary neighbor.Scientific exploration of Mars is thus of crucial value to our understanding of the solar system.The existence of abundant evidence for the f... Mars is not only our nearby but also the most Earth-like planetary neighbor.Scientific exploration of Mars is thus of crucial value to our understanding of the solar system.The existence of abundant evidence for the former presence of water on Mars demands further exploration for signs of life on our sister planet,and investigations that could shed light on conditions favorable to the origin of life.For nearly 60 years,humans have conducted orbitally-based remote sensing and in-situ surface exploration of Mars,leading to many significant scientific discoveries.But much remains to be done before we can be sure that we truly and fully understand Mars.Key research topics include the history of water on Mars and how that history relates to the planet’s habitable environment-past,present,and future;the distribution and evolution of waterbearing and evaporative salt minerals on the planet’s surface;the history of volcanic activity on Mars;the Martian magnetic field and its effect on the escape of water and atmosphere from the planet;interactions between the solar wind and the Martian atmosphere and ionosphere;atmospheric characteristics and climate change on Mars;and so on(Li CL et al.,2018;Liu JJ et al.,2018).Based on the above scientific questions about life,climate,and geology on Mars,the international planetary science community has formulated ambitious Mars exploration programs. 展开更多
关键词 MARS Tianwen-1 payload
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A discrete-event model to simulate the effect of truck bunching due to payload variance on cycle time, hauled mine materials and fuel consumption 被引量:2
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作者 A.Soofastaei S.M.Aminossadati +1 位作者 M.S.Kizil P.Knights 《International Journal of Mining Science and Technology》 SCIE EI CSCD 2016年第5期745-752,共8页
Data collected from truck payload management systems at various surface mines shows that the payload variance is significant and must be considered in analysing the mine productivity,energy consumption,greenhouse gas ... Data collected from truck payload management systems at various surface mines shows that the payload variance is significant and must be considered in analysing the mine productivity,energy consumption,greenhouse gas emissions and associated cost.Payload variance causes significant differences in gross vehicle weights.Heavily loaded trucks travel slower up ramps than lightly loaded trucks.Faster trucks are slowed by the presence of slower trucks,resulting in‘bunching’,production losses and increasing fuel consumptions.This paper simulates the truck bunching phenomena in large surface mines to improve truck and shovel systems’efficiency and minimise fuel consumption.The study concentrated on completing a practical simulation model based on a discrete event method which is most commonly used in this field of research in other industries.The simulation model has been validated by a dataset collected from a large surface mine in Arizona state,USA.The results have shown that there is a good agreement between the actual and estimated values of investigated parameters. 展开更多
关键词 Discrete-event model Simulation Truck bunching payload variance Cycle time Fuel consumption
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Mathematical modelling of translational motion of rail-guided cart with suspended payload 被引量:3
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作者 MITREV Rosen 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2007年第9期1395-1400,共6页
In this paper modelling of the translational motion of transportation rail-guided cart with rope suspended payload is considered. The linearly moving cart,driven by a travel mechanism,is modelled as a discrete six deg... In this paper modelling of the translational motion of transportation rail-guided cart with rope suspended payload is considered. The linearly moving cart,driven by a travel mechanism,is modelled as a discrete six degrees of freedom (DOF) dynamic system. The hoisting mechanism for lowering and lifting the payload is considered and is included in the dynamic model as one DOF system. Differential equations of motion of the cart elements are derived using Lagrangian dynamics and are solved for a set of real-life constant parameters of the cart. A two-sided interaction was observed between the swinging payload and the travel mechanism. Results for kinematical and force parameters of the system are obtained. A verification of the proposed model was conducted. 展开更多
关键词 Transportation rail-guided cart Travel mechanism Swinging payload Discrete dynamical model Mathematical model
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Introduction to the Payloads and the Initial Observation Results of Chang'E-1 被引量:4
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作者 SUN Huixian WU Ji +9 位作者 DAI Shuwu ZHAO Baochang SHU Rong CHANG Jin WANG Huanyu ZHANG Xiaohui REN Qiongying CHEN Xiaomin OUYANG Ziyuan ZOU Yongliao 《空间科学学报》 CAS CSCD 北大核心 2008年第5期374-384,共11页
Chang'E-1,the orbiter circling the moon 200km above the moon surface,is the first Chinese Lunar exploration satellite.The satellite was successfully launched on 24th October 2007.There are 8 kinds of scientific pa... Chang'E-1,the orbiter circling the moon 200km above the moon surface,is the first Chinese Lunar exploration satellite.The satellite was successfully launched on 24th October 2007.There are 8 kinds of scientific payloads onboard,including the stereo camera,the laser altimeter,the Sagnac-based interferometer image spectrometer,the Gamma ray spectrometer,the X-ray spectrom-eter,the microwave radiometer,the high energy particle detector,the solar wind plasma detector and a supporting payload data management system.Chang'E-1 opened her eyes to look at the moon and took the first batch of lunar pictures after her stereo camera was switched on in 20th November 2007.Henceforth all the instruments are successfully switched on one by one.After a period of parameter adjustment and initial check out,all scientific instruments are now in their normal operating phase.In this paper,the payloads and the initial observation results are introduced. 展开更多
关键词 有效载荷 嫦娥一号 空间技术 分光计 微波技术
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Type Design for Heavy-payload Forging Manipulators 被引量:5
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作者 GE Hao GAO Feng 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2012年第2期197-205,共9页
Heavy-payload forging manipulators are mainly characterized by large load output and large capacitive-load input.The relationship between outputs and inputs,which will greatly influence the control and the reliability... Heavy-payload forging manipulators are mainly characterized by large load output and large capacitive-load input.The relationship between outputs and inputs,which will greatly influence the control and the reliability,is the key issue in type design for heavy-payload forging manipulators.In this paper,a type design method by considering the incidence relationship between output characteristics and actuator inputs is presented and used to design the mechanism for forging manipulators.The concept of modeling method based on the outputs tasks is defined and investigated.The principle of type design from the viewpoints of the relationship between output characteristics and actuator inputs is discussed.An idea of establishing the incidence relationship between output characteristics and actuator inputs is proposed.The incidence relationship matrix between outputs and inputs is also given.The design flow is obtained,and the incidence relationship between outputs and inputs for heavy-payload forging manipulators is divided into three parts after detailed understanding of the functional properties.Four types of mechanisms for heavy-payload forging manipulators are given,and the corresponding spatial mechanical sketches are also drawn,some new designed mechanisms have been adopted by company or used as prototype.These novel forging manipulators which satisfy certain functional requirements provide an effective help for the design of forging manipulators and patent application. 展开更多
关键词 heavy-payload type design forging manipulators kinematic characteristics
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