毛细管平面辐射空调系统节能技术

目的如何实现空调系统更好的节能环保;方法介绍地源热泵工作原理以及它在毛细管平面辐射空调系统中的应用;结果指出将地源热泵技术用在毛细管平面辐射空调系统中;结论为空调系统的节能与环保提供了新的发展方向。     

混合管出口掺混距离对气流温度的影响

就弯曲混合管出口与模型出口之间相对距离的改变,对一体化红外抑制器模型出口混合气流温度的影响进行了数值模拟和分析.并通过实验,对出口间距变化时模型壁面的红外辐射场进行了测量.结果表明,延长混合管出口与模型出口之间相对距离,可以增加混合管热排气与冷却气流的掺混距离,使模型出口混合气流温度峰值下降约42%;但同时会使模型壁面在3～5μm波段和8～14μm波段的红外辐射强度有所增加.      

机载计算机ATE计量校准软件的研究与设计

全面有效地计量校准军用ATE,对保证其正确性有效性非常重要.设计开发ATE计量校准程序,可以实现ATE自动化整体原位校准,提高计量保障效率和测试质量.介绍了机栽计算机ATE计量校准软件的系统结构,重点讨论了计量校准程序结构和面向信号的程序开发方法,最后描述了计量校准程序流程和实现方法.     

氨质子化团簇红外振动光谱研究

运用Gaussian03W计算程序,在B3LYP／6—31G（d）方法水平上得到了氨质子化团簇（NH3）nH^＋（n=1～8）的最稳定构型,并对其相应红外振动光谱进行了研究。通过对红外振动光谱中谱峰位置与振动模式之间的关系的分析,发现光谱中的最强峰均来自于NH4^＋核中N—H键的反对称伸缩振动（n=2除外）。     

空间陀螺仪显式标定与隐式标定方法

针对航天器陀螺仪误差系数的标定问题,提出了显式与隐式两种标定方法。建立了显式标定与隐式标定方法的状态方程与测量方程,利用扩展Kalman滤波获得了陀螺仪误差系数的高精度估计,同时比较了显式标定与隐式标定的不同,仿真结果表明,在当前参数设置下,显式标定与隐式标定精度基本相同,两种方法得到的误差系数估计相对误差在10%以内,而隐式标定方法实现较为容易,但对航天器姿态测量精度较为敏感。     

Cosmic radiation exposure of aircraft occupants on simulated high-latitude flights during solar proton events from 1 January 1986 through 1 January 2008

From 1 January 1986 through 1 January 2008, GOES satellites recorded 170 solar proton events. For 169 of these events, we estimated effective and equivalent dose rates and doses of galactic cosmic radiation (GCR) and solar cosmic radiation (SCR), received by aircraft occupants on simulated high-latitude flights. Dose rate and dose estimates that follow are for altitudes 30, 40, 50, and 60 kft, in that order.     

利用质子强度变化对太阳质子事件进行短期预报方法初步研究

采用GOSE-10卫星4～9 MeV(P2),9～15 MeV(P3),15～40 MeV(P4),40～80 MeV(P5)能段上的质子通量数据,结合质子能谱,对太阳质子事件发生前各能谱参数的变化特征进行分析,详细介绍利用能谱参数的变化特征及能量E>10 MeV的质子通量数据对太阳质子事件进行预报的新方法,并运用这种方法对2002-2006年期间太阳质子事件进行了预报.预报结果显示,预报提前量最多达到100 h以上,对质子事件的报准率达97.5%,预报方法具备一定的有效性和实用性.      

The analysis of affections to the cold space calibration source of ChangE-1 payload Microwave Detector

ChangE-1 (CE-1) will be the first satellite of China in lunar orbit. Its Microwave Detector makes real-time and periodical calibration at high and low temperature points. The low brightness temperature calibration source will be provided by calibration antenna which is pointing towards the cold space.     

Influence of different atmospheric models and seeing effects on the nonlinear calibration

This paper describes a technique intended to improve calibration of vector magnetograms achieved by the spectral line Fei 5324.19 Å which was first described in detail by Hagyard and Kineke [Hagyard, M.J., Kineke, J.I., Improved method for calibrating filter vector magnetographs, Solar Phys., 158, 11–28, 1995.]. The technique attempts to compensate for nonlinear behavior of the measured linear and circular polarizations of the line as functions of inclination angle and field strength. This method depends on different atmospheric models. To the three different atmospheric models, the VAL-C quiet photosphere model, the Ding and Fang penumbra model and Allen umbral model, the circular polarization signal is directly linearly proportional to the longitudinal field strength in the range of 800 G, 1000 G and 1300 G, respectively. For the transverse field, however, this linear relationship holds over much smaller ranges which are 200 G, 300 G and 200 G. The improved method improves the accuracy in calibrating the polarization signals over a wide range of field strengths and inclination angles. With the seeing effects decreasing in the magnetic observation, the longitudinal fields and the transverse ones are underestimated. The differences in the zero-iterative longitudinal and transverse field are relatively minor, but differences in the multi-iterative longitudinal and transverse field can be as high as 260 G and 500 G. The improved calibration method is more sensitive to the seeing effects variation than the former calibration method.     

基于可观测度分析和模型预测的空间自标定方法

光纤陀螺以其优点适合空间飞行器定姿要求,但长期在轨飞行必须对光纤陀螺进行自标定。通常采用高维复杂陀螺模型计算实时性误差,而采用舍去状态量的降维模型影响系统定姿精度。针对这一问题,通过星敏感器观测,对高维陀螺模型进行可观测度分析,提出了一种基于模型预测的降维模型,将可观测度较低的状态作为模型误差进行预测估计,保证了系统精度并大大减小了计算量。半物理仿真结果表明此算法精度略高于高维模型自标定方法,计算量仅为高维模型的1/10,显著提高了系统的实时性。