卫星电磁兼容性设计技术

根据卫星上电子地器件多的特点，对气象卫星的电磁兼容性问题进行了研究，着重对卫星接地搭接、电磁屏蔽和电缆布线束的设计进行了分析。针对上述技术进行了讨论，提出了实施要求。经卫星在轨飞行验证，对FY－1C所进行的电磁兼容性设计是正确的。     

介绍几种液体燃料小滴燃烧的落塔试验方案

本文简要介绍微重力条件下液体燃料小滴燃烧研究中，所采用的几种塔试验方法及试验设备。给出了单滴静态燃烧，运动小滴的燃烧，小滴列燃烧等的试验装置图。     

基于Internet和Java3D的多机器人操作虚拟环境

网络传输时延的不确定性和机器人之间的有效协调是多机器人遥操作系统研究的关键问题.采用Java和Java3D技术构建了基于Internet的虚拟操作环境,改变了传统上基于视频信息作为反馈的操作模式,克服了网络传输时延对系统操作性能的影响.提出了基于虚拟向导的概念并加以实现,处于异端的操作者能够准确地预测其它操作者的操作意图并实现有效的协调动作.通过两个典型操作实例的分析,验证了系统的合理性与可行性.     

防护超高速碰撞破坏的材料设计

概述了超高速碰撞对空间飞行器的破坏效应，简述了防护超高速碰撞的薄板屏蔽方法。从冲击波传播规律出发，阐述了抗超高速碰掸破坏的防护材料的理论设计方法，提出了防护材料的基本结构模型。     

智能产品数据服务环境

提出了一种支持复杂工程系统多学科协同设计优化的产品数据管理方法及基于系统优化任务的智能产品模型数据组织模式。通过工程控制结构模型，定义了产品优化任务，并为设计任务自顶向下进行产品模型控制提供了途径。利用产品主模型技术实现数据的完整性，通过设计任务的语境模型产生数据高保真的分析视图以及关联数据环境实现产品主模型和分析模型的一致性。整个产品数据通过协作数据对象的封装，以WEB服务的形式，使优化设计人员通过网络透明地获取产品数据。为了支持基于INTERNET的协同产品开发，采用了基于OPENHSF的流格式作为产品数据的显示方式。     

强噪声环境试验的频谱模拟

评述了强噪声环境规范的发展和现有声源产生噪声的能力。讨论了噪声场频模拟的自支动控制系统并在计算机上进行了仿真，结果比较满意。     

Space Environment Prediction for SZ-4 and SZ-5

The Space Environment Prediction Center (SEPC) of the Center for Space Science and Applied Research of the Chinese Academy of Sciences (CSSAR, CAS)took on the mission of offering the space environment parameters which may be of use to the safety of manned spacecraft. In order to complete the space environment safety guarantee mission for SZ-4 and SZ-5, SEPC improved the space environment monitoring system, database system, prediction result display system, prediction implementation system, etc. For guaranteeing the safety of the airship and cosmonaut in the first manned SZ-5, flying experiment mission,SEPC developed the software for analyzing radiation dose and early-warning software for large debris collision with SZ-5. Three months before the flights of SZ-4 and SZ-5, SEPC began to predict the safe launch period in view of the space environment, and offered timely and valid reference opinions for selecting the safety period. Especially during the mission of SZ-5, SEPC analyzed the space high-energy environment in a pre-arranged orbit and abnormal orbit andevaluated the radiation dose which cosmonauts may encounter in space. The evaluation offered an important reference for cosmonaut safety and decisionmaking in the SZ-5 mission. The calculation of the distribution of large debris and the collision risk assessment at different orbit entry times for SZ-5 provided an important base for the superior department to make flight decisions.     

太空环境对肿瘤细胞生理特性的影响

将3种肿瘤细胞搭载于“神舟4号”的卫星返回舱内,经过7天太空飞行,回收后对存活细胞进行单克隆化,观察细胞形态,并测定了细胞周期、黏附力及细胞因子表达.结果显示,经太空飞行,小鼠黑色素瘤B16细胞的周期发生改变,G1期细胞明显增多(p<0.05),并表现多种细胞形态;人肺鳞癌细胞L78对血管内皮细胞黏附力明显减弱,但经传代培养其黏附力恢复且超过对照组细胞;Caski细胞IL-2、IL-8、TNF和TGF的表达均明显增加,而L78细胞上述4种细胞因子的表达均显著下降.结论,太空环境可影响肿瘤细胞的某些生理特性,但可否影响肿瘤细胞的免疫原性,仍需做进一步的实验.     

卫星介质深层充电中的主要物理问题

卫星介质深层充电效应是诱发地球同步轨道卫星运行故障和异常的重要因素之一，通过计算机模拟对介质深层充电的时间常数、电场特征、以及屏蔽、介质厚度和接地方式对充电所致最大电场的影响等主要物理问题进行了详细的分析，并给出了初步的防护措施．     

Long term and safe relative orbit design for heterogeneous spacecraft clusters

The problem of obtaining long term relative orbit configurations for spacecraft clusters with realistic operational considerations such as safety, station keeping and inter-spacecraft distances is addressed. Two different approaches are developed for station keeping and safety objectives. In the first approach, relative orbit configurations, or relative TLEs, are found minimizing deviations from reference mean orbit which would maximize the station-keeping objective. In second one, relative configurations are found from a reference initial condition by minimizing probability of collision, hence maximizing the safety objective, between the spacecraft in the cluster which are propagated numerically through a high precision orbit propagator. For the design optimization, a derivative free algorithm is proposed. Effectiveness of the approaches is demonstrated through simulations. Using this design framework, several configurations can be found by exploring the limits of the clusters in terms of spacecraft number, distance bounds and probabilities of collision for long time intervals.