三维体视投影图画法基础

主要介绍三维体视投影图的画法，指出作图的基本规律和图形的表现方法。     

基于三维有限元的火箭模态振型斜率预示方法研究

振型斜率火箭是姿控系统设计的重要参数,对飞行任务的可靠性与安全性有着至关重要的作用。依据全箭动特性的测量原理及参数定义,结合三维有限元建模方法和模型修正技术,全面考虑了速率陀螺、惯组安装位置处的局部刚度对振型和振型斜率的影响,建立了基于局部细节精细化建模的全箭模态振型斜率预示方法,并总结了3种不同的振型斜率提取方法,提高了振型斜率的预示精度。同时提供了三维模型振型一维化的方法,解决了使用三维有限元模型计算弹性运动方程式系数的难题。     

Shape control of spacecraft formation using a virtual spring-damper mesh

This paper derives a distance-based formation control method to maintain the desired formation shape for spacecraft in a gravitational potential field. The method is an analogy of a vir-tual spring-damper mesh. Spacecraft are connected virtually by spring-damper pairs. Convergence analysis is performed using the energy method. Approximate expressions for the distance errors and control accelerations at steady state are derived by using algebraic graph representations and results of graph rigidity. Analytical results indicate that if the underlying graph of the mesh is rigid, the convergence to a static shape is assured, and higher formation control precision can be achieved by increasing the elastic coefficient without increasing the control accelerations. A numerical exam-ple of spacecraft formation in low Earth orbit confirms the theoretical analysis and shows that the desired formation shape can be well achieved using the presented method, whereas the orientation of the formation can be kept pointing to the center of the Earth by the gravity gradient. The method is decentralized, and uses only relative measurement information. Constructing a distributed virtual structure in space can be the general application area. The proposed method can serve as an active shape control law for the spacecraft formations using propellantless internal forces.     

系留气球囊体外形优化研究

利用基于约束的Kanikdale修正算法,以及一套用于确定尾翼尺寸和系留缆绳外形的方法,并借助基于GA的GADO优化器,对系留气球囊体形状进行了优化研究。结果表明,通过多材料组合方式生成的囊体,其有效载重能力能够提升6.5%左右。     

A new inversion method of plasma density distribution of plasmasphere in the geomagnetic equatorial plane from IMAGE data

The plasma density distribution of plasmasphere in the geomagnetic equatorial plane can help us study the magnetosphere like plasmasphere, ionosphere and their kinetics. In this paper, we introduce a new inversion method, GE-ART, to calculate the plasma density distribution in the geomagnetic equatorial plane from the Extreme Ultraviolet (EUV) data of IMAGE satellite under the assumption that the plasma density is constant along each geomagnetic field line. The new GE-ART algorithm was derived from the traditional Algebraic Reconstruction Techniques (ART) in Computed Tomography (CT) which was different from the several existing methods. In this new method, each value of the EUV image data was back-projected evenly to the geomagnetic field lines intersected by this EUV sight. A 3-D inversion matrix was produced by the contributions of all the voxels contained in the plasmasphere covered by the EUV sensor. That is, we considered that each value of the EUV image data was relative to the plasma densities of all the voxels passed through by the corresponding EUV radiation, which is the biggest difference to all the existing inversion methods. Finally, the GE-ART algorithm was evaluated by the real EUV data from the IMAGE satellite.     

一种红外焦平面阵列相对光谱响应自动测试系统

目前测试红外焦平面阵列相对光谱响应参数时，需要人工测量波段中每个波长点的光谱响应，针对测试过程繁琐和测试时间长的问题，在基于现有的不同开发平台开发的单色仪和数据采集系统的基础上，利用动态链接库技术，研制了一种红外焦平面阵列相对光谱响应自动测试系统，该系统测试过程简化，自动化程度提高。经过对比分析，自动测试与人工测试结果具有较好的一致性，自动测试比人工测试更加可靠。     

支承座三工序复合冲压模具

介绍一种新型支承座三工步复合冲压模具的结构、工作原理、主要工作部件的设计技术和参数计算。使用此种模具，可以在一个工步中完成支承座毛坯的落料、冲孔和弯曲成形，生产效率高，工艺质量好。     

第十一届新加坡航展印象

简要介绍了第十一届新加坡航展的参展情况。通过参观访问深感军民用发动机市场竞争十分激烈。GE、PW、RR等公司均积极地参与了中国ARJ21新支线喷气客机选发的竞争,我国“新舟60”首次参展引起了国内外同行的关注。     

建立室内虚拟长度基线场的可行性探讨

提出了利用两平面反射镜多次反射来虚拟室外基线场,在室内完成检定光电测距仪及全站型电子速测仪测距部分的解决方案;在现有技术的层面上对该方案所面临的技术难题进行了探讨,对其可行性进行了论证;对该方案实施1000 m测长的不确定度进行了详细的分析和计算,得出了该方案完全可行的结论.     

发动机安装面振动分析

在某民用涡轮风扇发动机的持久试车过程中 ,出现了发动机后安装面振动异常的现象。针对这一故障现象进行了模拟计算分析 ,找出了故障的原因 ,提出了改进措施 ,部分措施得以应用 ,其效果良好。