线性调频脉冲压缩雷达仿真研究

文章分析了线性调频（LFM）脉冲压缩雷达的工作原理,对LFM信号及其匹配滤波输出信号进行了仿真,验证了理论分析的正确性,进而对LFM脉冲压缩雷达系统进行仿真,得出LFM信号可有效解决雷达作用距离与距离分辨率之间的矛盾。     

质量特性调整机构在航天器中的应用

质量特性调整机构具有成本低、体积小、重量轻、工作寿命长、可靠性高的优点,被用于在轨精确调整航天器的质量特性,从而确保航天器能够提供高精度的姿轨控以及部分有效载荷的正常工作。文章首先介绍了质量特性调整机构的设计原理和方案,以及在航天器中的应用情况和研究现状;其次对质量特性调整机构需要解决的关键技术进行了分析;最后对其在我国航天活动中的应用进行了展望。     

微小卫星推力器姿轨一体化控制技术研究

随着微小卫星的技术发展,采用微小卫星组网和轨道机动的需求越来越多。针对微小卫星重量轻、功耗低的特点,本文提出了基于推力器的姿轨一体化控制方案。该方案采用一个大推力器进行轨道控制,4个斜装小推力器兼顾轨道控制和姿态控制,不仅可在卫星轨道机动中实现三轴姿态控制,同时可提高控制系统的功能密度。采用Matlab仿真分析,给出了在卫星轨道机动中同时兼顾三轴姿态控制的仿真曲线。仿真结果表明:本文提出的控制策略具有很好的实用性。     

基于相位扰动的抗有源加性复合干扰技术

针对有源加性复合干扰,研究了基于相位扰动原理的干扰抑制方法。在结合LFM信号特征的基础上,对雷达发射信号的前后脉冲分别附加近似正交的扰动相位,再通过与前一脉冲重复周期相应的匹配滤波器将复合干扰中的欺骗干扰成分加强,并对脉冲压缩结果加以"惩罚",最后采用匹配滤波逆运算恢复出目标回波信号。     

复合纸板力学性能和应变率相关性测试与表征

为了研究复合纸板材料在不同应变率下的力学响应,利用万能材料试验机和高速率拉伸试验机进行了准静态和动态拉伸试验,同时利用高速摄像机和数字图像相关法(Digital image correlation,DIC)记录拉伸破坏过程和应变场。试验结果显示,纸板材料的拉伸力学性能和破坏机制具有明显的应变率相关性。随着应变率的增大,材料的拉伸强度显著增大,断裂应变在中应变率范围内也表现出明显的应变率效应。对比试验结果和3种应变率效应比表征模型的拟合结果,基于Cowper-Symonds表达式的表征模型,能够很好地描述纸板材料在中低应变率下的应变率效应。该模型对薄壁纸管能量吸收性能的模拟和理论研究,以及冲击防护结构设计提供了理论支撑。     

Design of Drilling and Riveting Multi-functional End Effector for CFRP and Aluminum Components in Robotic Aircraft Assembly

To fulfill the demands for higher quality,efficiency and flexibility in aviation industry,a multi-functional end effector is designed to automate the drilling and riveting processes in assembling carbon fiber reinforced polymer(CFRP)and aluminum components for a robotic aircraft assembly system.To meet the specific functional requirements for blind rivet installation on CFRP and aluminum materials,additional modules are incorporated on the end effector aside of the basic processing modules for drilling.And all of these processing modules allow for a onestep-drilling-countersinking process,hole inspection,automatic rivet feed,rivet geometry check,sealant application,rivet insertion and installation.Besides,to guarantee the better quality of the hole drilled and joints riveted,several online detection and adjustment measures are applied to this end effector,including the reference detection and perpendicular calibration,which could effectively ensure the positioning precision and perpendicular accuracy as demanded.Finally,the test result shows that this end effector is capable of producing each hole to a positioning precision within ±0.5 mm,aperpendicular accuracy within 0.3°,a diameter tolerance of H8,and a countersink depth tolerance of±0.01 mm.Moreover,it could drill and rivet up to three joints per minute,with acceptable shearing and tensile strength.     

Simulation of the land surface temperature from moon-based Earth observations

The land surface temperature (LST) is a key parameter for the Earth’s energy balance. As a natural satellite of the Earth, the orbital of the moon differs from that of current Earth observation satellites. It is a new way to measure the land surface temperature from the moon and has many advantages compared with artificial satellites. In this paper, we present a new method for simulating the LST measured by moon-based Earth observations. Firstly, a modified land-surface diurnal temperature cycle (DTC) method is applied to obtain the global LST at the same coordinated universal time (UTC) using the Moderate Resolution Imaging Spectroradiometer (MODIS) LST products. The lunar elevation angles calculated using the ephemeris data (DE405) from the Jet Propulsion Laboratory (JPL) were then applied to simulate the Earth coverage observed from the moon. At the same time, the modified DTC model was validated using in situ data, MODIS LST products, and the FengYun-2F (FY-2F) LST, respectively. The results show that the fitting accuracy (root-mean-square error, RMSE) of the modified DTC model is not greater than 0.72?°C for eight in situ stations with different land cover types, and the maximum fitting RMSE of the modified model is smaller than that of current DTC models. By the comparison of the simulated LST with MODIS and FY-2F LST products, the errors of the results were feasible and accredited, and the simulated global LST has a reasonable spatiotemporal distribution and change trend. The simulated LST data can therefore be used as base datasets to simulate the thermal infrared imagery from moon-based Earth observations in future research.     

法国海豚直升机的工艺特点

介绍了法国海豚直升机型号循序渐进发展,优先采用复合材料技术、注重产品质量检验等工艺特点。     

远海对抗中天基系统作用及发展状态分析

以信息化联合作战为主要特点的现代战争对天基系统的信息支援能力日益依赖,远海对抗以远离本土、网络协同、攻防兼备的特殊性,需要天基系统的支持更为全面和迫切。从远海对抗的内涵和任务需求出发,分析国外在远海对抗条件下天基系统如何为海洋作战平台提供及时、有效的信息支援,从而提出未来天基系统发展策略和设想。     

导弹垂直发射中二次流流场计算

本文应用Ｇｏｄｕｎｏｖ方法对导弹垂直发射系统的内流场进行了数值模拟，详细描述了导弹点火后二次流的形成及其对弹体的影响，为导弹的设计和发射系统的热防护提供参考。