活笥银粉中微量铜铁的测定

提出用空气－乙炔火焰原子吸收光谱法来测定银锌电池活性银粉中的微量铜铁，并对测定条件和干扰因素进行了综合考虑，该测定方法具有灵敏度、精确度高，干扰小，选择性和重现性好等优点。测定样品微量铜铁含量的相对标准偏差均小于１.5%(n=8）。标准加入回收率均在（９７.00-102.00)%(n=5)范围内，完全适用于银锌电池活性银粉中微量铜铁含量的控制和样品系统分析，实际应用中取得了很好的效果。     

一种不规则封闭形状的轮廓跟踪算法

论述了一种对不规则封闭形状的快速轮廓跟踪算法，提出了一种用于确定轮廓下一搜索点及判断轮廓走向的二维坐标算子，使得轮廓跟踪的搜索时间大为减少，提高了图象处理的实时性。用该算法编制的程序能适应各种形状的跟踪要求。     

利用光纤电容液滴分析仪测量液体折射率的研究

光纤电容液滴分析仪(FCDA:Fiber-capacitive Drop Analyzer)是一种用于液体特性研究的新型仪器,该仪器利用光纤液滴分析技术和电容液滴分析技术制成特殊的液滴传感器,获取经过液滴的光强信号随液滴生长变化的规律,得到反映液体综合特性的“液滴指纹图”。该仪器具有测量液体的物理特性参数的能力。本文就利用光纤电容液滴分析仪在液体折射率的测量方面进行了研究,利用线性关系来测量不同浓度的酒精的折射率,并给出了结果的误差分析。     

低RCS齿形挂架参数选择研究

常规飞机的机翼与外挂架构成90°的二面角,成为飞机侧向的重要散射源.为求在不改变机体结构的前提下减缩飞机侧向RCS,采用齿形方案改变了挂架外形,消除了直角二面角结构,削弱了耦合效应.计算结果显示,改形的国产某型战斗机的机翼-外挂架结构的RCS在侧向重点姿态角内降低了9~13dBsm,证明了齿形改形方案能明显改善飞机侧向的耦合散射效应.在计算过程中使用了射线追踪法.      

一种空中交通图象特征匹配方法

提出了一种确定飞机类型的新方法。通过 机外型和结构特征，利用空间投影理论建立了飞机投影图形与飞机姿态角之间的关系。通过该关系方程，有效地识别了飞机姿态角。利用已有的飞机型的投影图特征与实际飞机飞行图像特征之间的误差，根据最小方差进行了模型匹配。利用ＣＣＤ系统图像仿真结果表明，所提出的方法是有效的。     

Exploration life support technology challenges for the Crew Exploration Vehicle and future human missions

As NASA implements the U.S. Space Exploration Policy, life support systems must be provided for an expanding sequence of exploration missions. NASA has implemented effective life support for Apollo, the Space Shuttle, and the International Space Station (ISS) and continues to develop advanced systems. This paper provides an overview of life support requirements, previously implemented systems, and new technologies being developed by the Exploration Life Support Project for the Orion Crew Exploration Vehicle (CEV) and Lunar Outpost and future Mars missions. The two contrasting practical approaches to providing space life support are (1) open loop direct supply of atmosphere, water, and food, and (2) physicochemical regeneration of air and water with direct supply of food. Open loop direct supply of air and water is cost effective for short missions, but recycling oxygen and water saves costly launch mass on longer missions. Because of the short CEV mission durations, the CEV life support system will be open loop as in Apollo and Space Shuttle. New life support technologies for CEV that address identified shortcomings of existing systems are discussed. Because both ISS and Lunar Outpost have a planned 10-year operational life, the Lunar Outpost life support system should be regenerative like that for ISS and it could utilize technologies similar to ISS. The Lunar Outpost life support system, however, should be extensively redesigned to reduce mass, power, and volume, to improve reliability and incorporate lessons learned, and to take advantage of technology advances over the last 20 years. The Lunar Outpost design could also take advantage of partial gravity and lunar resources.     

Study of satellite retrieved CO2 and CH4 concentration over India

This paper reports a study of spatial and temporal variations of columnar averaged concentration of CO₂ and CH₄ over India using SCanning Imaging Absorption spectroMeter for Atmospheric CHartographY (SCIAMACHY) and Greenhouse gas Observing SATellite (GOSAT) data. Comparison of these data with the global view National Oceanic and Atmospheric Administration (NOAA) land data and also location specific flask data is made. The temporal variation in column averaged global CO₂ is similar to that over India and it is also similar to the NOAA surface flask data and global view. The variation in NOAA surface CH₄ is location dependent and its global view appears to vary seasonally in opposite phase with the column averaged CH₄ values from satellites, reflecting the limited comparability of surface and column averaged data. Over India the CO₂ maximum is in May and minimum in August/September while for CH₄ the maximum is in September and minimum in February/March. The seasonal variation of CH₄ over India is correlated with the eastern coastal rice cultivation.     

区域覆盖特殊椭圆轨道星座优化设计

分析了椭圆轨道的优良特性,它可集中覆盖地面上某一指定纬度带或区域.阐述了临界倾角太阳同步回归轨道这种特殊椭圆轨道的设计方法,总结了其轨道要素的计算步骤.探讨了临界倾角太阳同步回归轨道星座的设计思路,指出了影响星座对目标覆盖性能的关键参数是各个卫星通过目标上空的时刻.介绍了用遗传算法进行星座优化设计的数学模型,利用遗传算法进行了优化设计.讨论了优化结果的统计规律,符合该规律的星座就是本文所研究的特殊椭圆轨道星座,星座性能分析结果表明这种星座适用于区域覆盖.      

基于曲线合成插补理论的慢走丝线切割反向回退功能设计

从理论上和实践上论述了具有丝半径补偿功能的曲线合成插补理论。该理论直接利用轮廓曲线和丝圆的信息，不需计算等距曲线．间接实现任意直线和二次曲线的等距曲线的插补，有效地避免了传统计算等距曲线产生的计算误差，简化了数控机床控制程序设计，提高了机床的控制精度。并研究了基于曲线合成插补理论的慢走丝线切割机床反向回退指令的形成、控制程序设计，并在慢走丝线切割机床数控系统设计中得到了应用。