一种激光多普勒测速仪辅助捷联惯导在线标定方法

针对惯组长期贮存过程中陀螺和加速度计零偏漂移的问题, 提出了一种利 用激光多普勒测速仪辅助捷联惯导的在线标定方案。给出了包括激光多普勒测速仪安装 误差角和惯组安装误差角的航位推算误差方程。基于航位推算误差方程建立了闭环卡尔 曼滤波器,对惯组零偏误差、激光多普勒测速仪安装误差角和惯组方位安装误差角进行 在线标定。仿真结果表明,加速后激光多普勒测速仪安装误差角和惯组方位安装误差角 得到估计;方位角改变后惯组零偏误差也得到估计。该方法允许跑车前不用综合标定, 直接装订前一次的安装角参数,缩短了准备时间。     

动态扭矩遥感测试系统校准方法研究

介绍了一种动态扭矩遥感测试系统的工作原理及其应用,提出了针对该类动态扭矩测试系统的校准原理,并介绍了具体的校准方法.     

基于试飞数据的飞行模拟器气动模型校核

为了提高飞行模拟器气动模型模拟的逼真度和置信度,提出了一种模拟器气动模型校核方法。采用先校核纵向、再校核横航向,先校核稳态、再校核动态的思路,通过对比试飞数据与仿真模型相关参数来修正引起偏差的气动导数项;综合分析不同状态点修正系数存在的统计规律,形成可用于飞行仿真解算的气动参数修正模型。试飞数据验证表明,校核后的仿真气动模型能满足模拟器客观测试规范要求,显著提高了气动模型模拟的逼真度。     

热敏电阻元件低温校准方法研究

介绍了热敏电阻元件低温校准系统的校准原理及校准关键技术,以MF5602型和MF5604型负温度系数热敏电阻元件为例,对校准系统和关键技术、校准方程以及数据拟合方法进行了研究,提出了火箭发动机用热敏电阻元件在低温环境下的校准方法.     

Geodetic Methods for Calibration of GRACE and GOCE

It is beyond doubt that calibration and validation are essential tools in the process of reaching the goals of gravity missions like GRACE and GOCE and to obtain results of the highest possible quality. Both tools, although general and obvious instruments for any mission, have specific features for gravity missions. Therefore, it is necessary to define exactly what is expected (and what cannot be expected) from calibration and what from validation and how these tools should work in our case. The general calibration and validation schemes for GRACE and GOCE are outlined. Calibration will be linked directly to the instrument and the measurements whereas validation will be linked to data derived from the original measurements. Calibration includes on-ground, internal, and external calibration as well as error assessment. The calibration phase results in corrected measurements along with an a posteriori error model. Validation of e.g. calibrated measurements or geoid heights means checking against independent data to assess whether there are no systematic errors left and/or whether the error model describes the true error reasonably well. Geodetic methods for calibration typically refer to external calibration and error assessment, and will be illustrated with an example. This revised version was published online in August 2006 with corrections to the Cover Date.     

动静载综合参数校准装置及应用

介绍了一种基于现场校准的动静载综合参数校准装置。本装置具有测量精度高、重复性好、智能化、操作简单、用户可自由扩展等优点。     

对检定与校准、检定规程与校准规范的再认识

近年来,对检定与校准、检定规程与校准规范的区别及各自的重要性,不少资料和文章都做了叙述与讨论,本文结合工作实践,从测量器具的检定与校准、检定规程与校准规范的编写等方面,谈谈对其再认识。     

基于刃边法的航天光学遥感器在轨MTF测试研究

调制传递函数（MTF,Modulation Transfer Function）在轨测试是监测航天光学遥感器在轨运行性能的重要指标。准确把握遥感成像系统MTF在运行过程中的变化,关系到遥感数据资源的合理及有效利用。文章对刃边法测试MTF的原理及仿真算法进行了阐述,重点对刃边倾角、辐射定标和刃边图像的对比度对MTF测试精度的影响进行了仿真分析。     

Transponder calibration of the Envisat RA-2 altimeter Ku band sigma naught

Although the history of spaceborne altimeters goes back to the early seventies, the absolute calibration of the backscattering coefficient has never been deeply investigated. This information has been primarily used to infer the wind speed via an empirical model, and the intercalibration among different satellite altimeters has revealed to be suitable for this purpose, being the wind retrieval based on an empirical relationship. As far as Ku band system is concerned, the sigma naught absolute calibration of the Envisat altimeter (RA-2) has been performed using an active reference target provided by a transponder. This has been exploited during the 6-month Commissioning phase to generate early calibration results. In order to monitor the RA-2 backscatter calibration during the Envisat lifetime, a continuous calibration effort has been carried out by operating the transponder as much as possible. This paper aims to review the entire effort for calibrating the RA-2 sigma naught measurements, which lasted for almost seven years. It presents in detail the adopted methodology and the final outcome of the activity, providing the users with the correction (bias) to get the calibrated sigma naught and analyzing its stability during almost the entire Envisat lifetime. Specifically, it is concluded that the RA-2 backscatter measurements were quite stable, even if a bias of about 1 dB should be considered with respect to the actually released product. Some small changes in the bias as function of time can be identified during most of the Envisat lifetime, consisting in a slight increase in the first two years, followed by a more stable period and a final drop observed at the end of 2009, until the conclusion of the calibration activity (corresponding to the change in Envisat orbit).     

超声波螺栓测量仪校准方法探索

针对超声波螺栓测量仪无法校准而影响实际使用的问题,提出了一种基于比较法的校准方法,为此类仪器的有效校准做了有益的探索。