一种硅角速率传感器的误差模型

微型传感器和高效信号处理之间的结合对于获得导航应用中所需的技术指标是至关重要的。文中概述了一种微机械硅角速率传感器的性能，表明它的主要缺陷是由一项重要的偏置漂移构成。本文建立了它的误差模型并且将它应用在基于卡尔曼滤波的修正运算之中。     

一次历史性的民间飞行活动

十一月六日 ,在北京应是深秋初冬 ,良乡机场的银杏树叶已完全金黄 ,晴朗的天空加之无风 ,天气形成的气温使人感到十分舒适 ,这无疑也是一个十分适宜于轻型飞机飞行的天气。1997年 11月 6日上午 10时 30分 ,一架海燕 650 B和一架蜜蜂 11轻型飞机编队通过跑道上空 ,解散后平稳着陆 ,一小时后 ,一架蜜蜂 3超轻型飞机通过跑道 ,在中央电视台预先架设好的地面摄像机上空低空盘旋 ,然后稳健地降落在跑道中央 ,它的最后降落 ,宣告了我国一次历史性的、极为艰巨的而又十分成功的民间长途飞行活动——′97飞向北京飞行活动的圆满结束。′97飞向北京…     

A hydrothermal system associated with the Siljan impact structure, Sweden--implications for the search for fossil life on Mars

The Siljan ring structure (368 +/- 1.1 Ma) is the largest known impact structure in Europe. It isa 65-km-wide, eroded, complex impact structure, displaying several structural units, including a central uplifted region surrounded by a ring-shaped depression. Associated with the impact crater are traces of a post-impact hydrothermal system indicated by precipitated and altered hydrothermal mineral assemblages. Precipitated hydrothermal minerals include quartz veins and breccia fillings associated with granitic rocks at the outer margin of the central uplift, and calcite, fluorite, galena, and sphalerite veins associated with Paleozoic carbonate rocks located outside the central uplift. Two-phase water/gas and oil/gas inclusions in calcite and fluorite display homogenization temperatures between 75 degrees C and 137 degrees C. With an estimated erosional unloading of approximately 1 km, the formation temperatures were probably not more than 10-15 degrees C higher. Fluid inclusion ice-melting temperatures indicate a very low salt content, reducing the probability that the mineralization was precipitated during the Caledonian Orogeny. Our findings suggest that large impacts induce low-temperature hydrothermal systems that may be habitats for thermophilic organisms. Large impact structures on Mars may therefore be suitable targets in the search for fossil thermophilic organisms.     

Fluid inclusion studies of chemosynthetic carbonates: strategy for seeking life on Mars

Fluid inclusions in minerals hold the potential to provide important data on the chemistry of the ambient fluids during mineral precipitation. Especially interesting to astrobiologists are inclusions in low-temperature minerals that may have been precipitated in the presence of microorganisms. We demonstrate that it is possible to obtain data from inclusions in chemosynthetic carbonates that precipitated by the oxidation of organic carbon around methane-bearing seepages. Chemosynthetic carbonates have been identified as a target rock for astrobiological exploration. Other surficial rock types identified as targets for astrobiological exploration include hydrothermal deposits, speleothems, stromatolites, tufas, and evaporites, each of which can contain fluid inclusions. Fracture systems below impact craters would also contain precipitates of minerals with fluid inclusions. As fluid inclusions are sealed microchambers, they preserve fluids in regions where water is now absent, such as regions of the martian surface. Although most inclusions are < 5 microns, the possibility to obtain data from the fluids, including biosignatures and physical remains of life, underscores the advantages of technological advances in the study of fluid inclusions. The crushing of bulk samples could release inclusion waters for analysis, which could be undertaken in situ on Mars.     

Arm end-point trajectories under normal and micro-gravity environments

The purpose of the present experiment was to study the way in which the CNS represents gravitational force during vertical arm pointing movements. Movements in upward and downward directions were executed by two cosmonauts in normal-gravity and weightlessness. Analyses focused upon finger kinematics in the sagittal plane. In normal-gravity, downward direction movements showed smaller curvatures and greater relative times to peak velocity (AT/MT) when compared with upward direction movements. Data from the weightlessness experiments showed that whilst downward movements decreased their curvature during space flight, curvatures of upward movements changed slightly. Furthermore, AT/MT was modified during the first days in micro-gravity for both directions, recovering, however, to pre-flight values after 18 days in space. Results from the present study, provide evidence that gravitational force is centrally treated constituting an important component of the motor plan for vertical arm movements.     

KINETICS OF δ PHASE PRECIPITATION IN COLD ROLLED INCONEL 718 ALLOY

ＫＩＮＥＴＩＣＳＯＦδＰＨＡＳＥＰＲＥＣＩＰＩＴＡＴＩＯＮＩＮＣＯＬＤＲＯＬＬＥＤＩＮＣＯＮＥＬ７１８ＡＬＬＯＹＬｉｕＷｅｎｃｈａｎｇ，ＹａｏＭｅｉ（ＹａｎｓｈａｎＵｎｉｖｅｒｓｉｔｙ，Ｑｉｎｈｕａｎｇｄａｏ，Ｃｈｉｎａ，０６６００４）ＬｉｕＲｕｎｇ...     

计划概述

1975年3月18、19、20日,在海军海面武器中心白橡树实验所举行了汇报海军再入技术计划的会议。海军再入技术计划是海军海上系统司令部(SEA-035)主持的一项探索性发展计划。该计划的目的是为今后的先进战略武器系统的再入体开展航空弹道学、材料和结构技术的研究。在整个再入技     

高分子湿敏电容的设计

从传感器功能要求出发,阐述了高分子湿敏电容正向设计规则.介绍了电容型高分子湿敏元件的感湿机理、元件结构、工艺过程和感湿材料设计方法,同时以应用示例给予说明.     

随机子阵阵列的旁瓣电平和宽带特征

本文扩展了随机天线阵列的概念。介绍了三种新型的阵列几何图形，它们既具有随机阵列的宽带宽性能，几何图形也更简单，因而更适宜于低成本应用。对随机子阵的周期阵列、周期旋转随机子阵阵列和随机旋转随机子阵阵列的性能都进行了统计性的表征。结果表明子阵旋转能够降低天线阵排列因子的旁瓣电平。文中给出了一个设计过程的例子来说明天线阵排列因子的计算。     

富氢燃气与空气低压补燃特性研究

氢氧火箭发动机在飞行过程中排出富氢燃气与周围低压空气发生补燃,直接改变发动机周围的热环境,影响发动机各组件性能。通过试验及仿真研究了不同燃气温度、燃气组分对于富氢燃气低压补燃特性的影响。富氢燃气与空气的低压补燃试验表明:常压下富氢燃气温度高于932 K时发生补燃,低于877 K时不发生补燃;富氢燃气温度高于950 K,环境压力60 kPa时富氢燃气发生补燃,30 kPa时不发生补燃;仿真与试验对比分析发现最大化学反应速率超过10~(-9)情况下能观测到宏观的富氢燃气与空气的补燃现象,燃气温度和氢气含量越高,其与空气发生补燃的临界压力越低。当压力低于10 k Pa时,燃气温度1 200 K,氢气含量87. 4%也无法与空气发生补燃。