Motion prediction of a non-cooperative space target

Capturing a non-cooperative space target is a tremendously challenging research topic. Effective acquisition of motion information of the space target is the premise to realize target capture. In this paper, motion prediction of a free-floating non-cooperative target in space is studied and a motion prediction algorithm is proposed. In order to predict the motion of the free-floating non-cooperative target, dynamic parameters of the target must be firstly identified (estimated), such as inertia, angular momentum and kinetic energy and so on; then the predicted motion of the target can be acquired by substituting these identified parameters into the Euler’s equations of the target. Accurate prediction needs precise identification. This paper presents an effective method to identify these dynamic parameters of a free-floating non-cooperative target. This method is based on two steps, (1) the rough estimation of the parameters is computed using the motion observation data to the target, and (2) the best estimation of the parameters is found by an optimization method. In the optimization problem, the objective function is based on the difference between the observed and the predicted motion, and the interior-point method (IPM) is chosen as the optimization algorithm, which starts at the rough estimate obtained in the first step and finds a global minimum to the objective function with the guidance of objective function’s gradient. So the speed of IPM searching for the global minimum is fast, and an accurate identification can be obtained in time. The numerical results show that the proposed motion prediction algorithm is able to predict the motion of the target.     

航天器分裂体或抛射物的轨道形成和演化

由卫星和碎片爆炸或相互间碰撞所产生的分裂体,或由在轨航天器向外抛射所产生的抛射物,对空间环境的影响正日益增大。对它们轨道形成和演化的研究可以为分析空间解体事件提供一种有效方法。本文利用Kep-ler运动积分以及受摄二体问题的分析解,建立了分裂体或抛射物的轨道形成及其演化与分裂或抛射速度之间的关系,从而为理解以各个方向、不同大小的速度分裂或抛射的物体的轨道演化特征提供理论依据。文章最后通过数值验证表明了该方法的有效性。     

我国航空运输需求价格弹性测算

根据经济学理论,同时结合我国航空运输的特点,通过引入我国GDP和我国航空运输每运输吨公里收入两个变量,利用线性回归分析的方法建立了我国航空运输需求函数,并根据需求函数绘制了我国航空运输需求曲线,然后根据需求函数和需求曲线测算了我国航空运输需求价格弹性值。最后,对本研究需要改进的方面进行了分析和总结。     

三轴台中框轴系静态设计与装调(下)

４内、中框轴线垂直度的调整一般来说，内中框轴相互垂直度的精度主要取决于中框架安装内框轴承的上下两孔的轴线与中框轴安装端面的平行度、与上、下孔、左、右止口的同轴度，即取决于中框架的加工精度，对于高精度的要求（１″），受加工机床精度的局限，不能满足精度要...     

一种在理论模线控制下的飞机结构立体图快速画法

绘制飞机结构立体图通常会涉及到飞机外形。由于飞机外形复杂，用传统方法绘制与外形有关的立体图不仅速度慢，而且局限性大。本文介绍一种在理论模线控制下的飞机结构立体图快速画法。     

The Balloon Array for RBSP Relativistic Electron Losses (BARREL)

BARREL is a multiple-balloon investigation designed to study electron losses from Earth’s Radiation Belts. Selected as a NASA Living with a Star Mission of Opportunity, BARREL augments the Radiation Belt Storm Probes mission by providing measurements of relativistic electron precipitation with a pair of Antarctic balloon campaigns that will be conducted during the Austral summers (January-February) of 2013 and 2014. During each campaign, a total of 20 small (～20 kg) stratospheric balloons will be successively launched to maintain an array of ～5 payloads spread across ～6 hours of magnetic local time in the region that magnetically maps to the radiation belts. Each balloon carries an X-ray spectrometer to measure the bremsstrahlung X-rays produced by precipitating relativistic electrons as they collide with neutrals in the atmosphere, and a DC magnetometer to measure ULF-timescale variations of the magnetic field. BARREL will provide the first balloon measurements of relativistic electron precipitation while comprehensive in situ measurements of both plasma waves and energetic particles are available, and will characterize the spatial scale of precipitation at relativistic energies. All data and analysis software will be made freely available to the scientific community.     

小型高精度重力计的微装配技术

以重力计的重力摆锤装配为例介绍了微装配系统的组成、夹持技术、力反馈技术.采用微装配技术以及进行装配工艺研究,重力摆锤的装配成活率由以前的25%提高到了81%,并降低了对工人的技能要求.     

论“异化”与“归化”翻译策略

论文探讨了"异化" 与"归化"的中外文渊源及其内涵,对比分析了"异化"与"归化"和"直译"与"意译"的辩证关系,并进一步预测了"异化" 与"归化"的发展趋势.这两对术语的界定与区分属于范畴基础研究,这种研究有助于范畴的规范化及翻译理论体系的建立,也有利于指导翻译教学与实践.     

不同回火温度对冶金锯片用钢65Mn力学性能的影响

利用力学性能测试及热处理分析，在360℃-540℃之间对冶金锯片用钢65Mn进行了连续回火处理。结果显示：随着回火温度的升高，试样的强度及硬度连续下降。在400—420℃之间，发现了回火脆性，冲击值、断面收缩率和延伸率发生明显变化。实验结果为预防锯片工作过程中的失效提供了技术参考。