红外地球敏感器的高截止度新型红外滤光片的设计

高截止度新型红外滤光片是三轴稳定卫星红外地球敏感器的关键件之一。文章介绍了用等效折射率概念设计这种滤光片的方法 ,讨论并给出了膜系设计和研制的结果 ,简介了镀膜的工艺技术 ,并与国内外同类滤光片的光学特性进行了比较 ,试验表明新型红外滤光片的膜系设计是成功的。     

红外调焦仪及其装调技术

介绍某型号红外光学系统装配专用红外调焦仪的结构与工作原理。着重论述其组成部分的关键装调技术、要求与方法以及有关示意图。考核表明，该红外调焦仪的性能和装配精度可满足要求。     

红外热波成像法测量薄板局部换热系数

通过连续激光调制对薄板试样进行局部周期加热，采用红外扫描测温技术记录动态温度分布。利用博里叶变换分析温度基波相位和幅值变化，进而推算壁面的局部换热系数。介绍了该方法的测量原理，在风洞中对两种不同厚度的薄板进行了实验研究，并对实验结果进行了分析和讨论。     

红外制导系统仿真技术的现状与发展

本文以国内、外红外制导武器的发展为基础，论述了红外制导系统仿真技术的特点、现状和今后的发展趋势。强调了对复合制导仿真研究的重要性。     

红外地平仪姿态测量误差模型

分析得出地球扁率和红外辐射是扫描式红外地平仪测量误差的主要原因。针对地球扁率，基于方位角的确定，分别给出了滚动角和俯仰角的测量误差模型。在地球红外辐射方面，给出了确定地平仪扫人、扫出点位置的方法，进而给出地球红外辐射误差的计算方法。最后，通过算例，给出了有关仿真结果，对方法的有效性进行了验证。     

CBERS-1卫星红外多光谱扫描仪图像预处理方法

文章介绍了中国和巴西联合研制的资源一号卫星 (CBERS_1)上的有效载荷之一 - -红外多光谱扫描仪 (IRMSS)图像数据的处理 ,包括错位校正、相对辐射校正和去除噪声等处理过程。     

红外／紫外双色制导系统数学模型及数字仿真

介绍了便携式防空导弹双色导引头中所采用的数字式控制系统代替传统的模拟式控制系统的方法。对导引头和自动驾驶仪部分的数学模型作了简化，并作了全弹道数字仿真。仿真结果表明，该双色制导体系设计方便，抗干扰能力强等。     

Feasibility of developing an ionospheric E-region electron density storm model using TIMED/SABER measurements

We present a new technique for improving ionospheric models of nighttime E-region electron densities under geomagnetic storm conditions using TIMED/SABER measurements of broadband 4.3 μm limb radiance. The response of E-region electron densities to geomagnetic activity is characterized by SABER-derived NO⁺(v) 4.3 μm Volume Emission Rates (VER). A storm-time E-region electron density correction factor is defined as the ratio of storm-enhanced NO⁺(v) VER to a quiet-time climatological average NO⁺(v) VER, which will be fit to a geomagnetic activity index in a future work. The purpose of this paper is to demonstrate the feasibility of our technique in two ways. One, we compare storm-to-quiet ratios of SABER-derived NO⁺(v) VER with storm-to-quiet ratios of electron densities measured by Incoherent Scatter Radar. Two, we demonstrate that NO⁺(v) VER can be parameterized by widely available geomagnetic activity indices. The storm-time correction derived from NO⁺(v) VER is applicable at high-latitudes.     

On the measurements of the moon’s infrared temperature and its relation to the phase angle

Radiometric measurements of the thermal radiation originating from the moon’s surface were obtained using an infrared detector operating at wavelengths between 8 and 14 μm. The measurements cover a full moon cycle. The variation of the moon’s temperature with the lunar phase angle was established. The lunar temperatures were 391 ± 2.0 K for the full moon, 240 ± 3.5 K for the first quarter, and 236 ± 3 K for the last quarter. For the rest of the phase angles, the lunar temperature varied between 170 and 380 K. Our results are comparable with those obtained previously at these phase angles. For the new moon phase, the obtained temperature was between 120 and 133 K. With the exception of the new moon phase, our measurements at all the phase angles were consistent with those obtained using Earth-based data and those obtained by the Diviner experiment and the Clementine spacecraft. At the new phase, our measurements were comparable with those obtained from the ground but were significantly higher than those obtained by the Diviner and Clementine data. We attribute this inconsistency to either the calibration curve of our detector, which does not perform well at very low temperatures, or to infrared emission from the atmosphere. A simple linear model to predict the lunar temperature as a function of the phase angle was proposed. The experimental errors that affect the measured temperatures are discussed.