On-orbit determination and adjustment of electrostatic accelerometer lever arm

In order to ensure the proof mass center of electrostatic accelerometer (EA) is fixed at the center of gravity of satellite as precisely as possible, an on-orbit determination and adjustment strategy of EA lever arm is presented in this paper. The EA lever arm is determined using the observations of EA, gyro and magnetometer first. Then it is adjusted by screw slider mechanism. The simulation results demonstrate that the proposed strategy can be carried out several times to yield better accuracy. Meanwhile, the optimal geographic location for EA lever arm determination along each axis is found.     

INR系统用于静止轨道高姿态精度卫星的分析

图像导航与配准(INR)系统是气象卫星的一项核心技术,INR采用系统分析的方法保证了卫星成像设备的指向精度和稳定性。文章介绍了INR的概念和主要处理过程,对INR系统的扰动源分析和技术方法进行了简要描述。结合天基红外高轨卫星、高分辨率成像卫星和激光通信卫星等高姿态精度卫星的系统组成和载荷技术特点,分析了INR技术方法在这些卫星上应用的可行性,并根据这三类卫星的载荷特点提出了INR具体应用的适应性修改,可以为卫星任务分析、系统设计提供参考和借鉴。     

Performance improvement for constellation SAR using signal processing techniques

A new concept of spaceborne synthetic aperture radar (SAR) implementation has recently been proposed - the constellation of small spaceborne SAR systems. In this implementation, several formation-flying small satellites cooperate to perform multiple space missions. We investigate the possibility to produce high-resolution wide-area SAR images and fine ground moving-target indicator (GMTI) performance with constellation of small spaceborne SAR systems. In particular, we focus on the problems introduced by this particular SAR system, such as Doppler ambiguities, high sparseness of the satellite array, and array element errors. A space-time adaptive processing (STAP) approach combined with conventional SAR imaging algorithms is proposed which can solve these problems to some extent. The main idea of the approach is to use a STAP-based method to properly overcome the aliasing effect caused by the lower pulse-repetition frequency (PRF) and thereby retrieve the unambiguous azimuth wide (full) spectrum signals from the received echoes. Following this operation, conventional SAR data processing tools can be applied to focus the SAR images fully. The proposed approach can simultaneously achieve both high-resolution SAR mapping of wide ground scenes and GMTI with high efficiency. To obtain array element errors, an array auto-calibration technique is proposed to estimate them based on the angular and Doppler ambiguity analysis of the clutter echo. The optimizing of satellite formations is also analyzed, and a platform velocity/PRF criterion for array configurations is presented. An approach is given to make it possible that almost any given sparse array configuration can satisfy the criterion by slightly adjusting the PRF. Simulated results are presented to verify the effectiveness of the proposed approaches.     

沿曲面交线多坐标数控加工的算法研究

分析了曲面交线加工中刀具的偏置类型,提出了新的交线加工刀位轨迹生成算法。该算法利用曲面跟踪求交算法计算两曲面交线,并根据交线处曲面局部微分几何性质推算刀具的初始位置,然后采用牛顿迭代算法精确刀位。该算法的优点是能够精确控制刀具与曲面的加工误差,可处理单支点、双支点偏置情况下球头刀、平底刀、圆角刀的交线域加工,算法稳定、统一。     

离散气膜孔下游边界层的实验研究

“Ｘ”型热线测量了离散气膜孔下游边界层内的湍流量,将热线探头绕轴转三个角方位以感受三维湍流场信息。结果表明,边界层内湍动能分布呈反“Ｓ”形,吹风比和孔排数对参数分布有重要影响,这种影响在很长距离上不消失,所以,常用的ｋ－ε模型不经修正不能正确预计这类边界层的发展。     

多状态故障树分析

通常故障树分析(FTA)只考虑底事件和顶事件的两状态(故障或成功)。实际工作中迫切需要考虑多种故障模式和不同故障程度(多状态)问题。本文首先讨论多元布尔逻辑,然后提出多状态故障树的不交型布尔代数分析法,最后介绍一个把统计相依事件化成多状态元件的故障树分析例子。     

自旋卫星转速控制系统的多状态非单调关联故障树定性分析

<正> 一、概述朱毅麟同志在《用故障树法分析自旋卫星转速失控》一文中,讨论了自旋卫星转速无限制地增加导致卫星失败的故障,考虑了自旋卫星设切向发动机锁定机构和设反向减转发动机的保护措施。这是一项有意义的分析工作。鉴于自旋卫星转速控制系统具有多状态非单调关联系统的性质,而上文只作为两状态单     

含多裂纹连接结构损伤容限试验研究

 针对机翼典型对接结构,进行了平板空孔试样和螺栓搭接件在等幅谱及飞－续－飞谱下的多裂纹损伤容限试验,通过该试验开展多裂纹开裂模式及多裂纹扩展规律的试验研究,为多裂纹断裂力学理论分析、多裂纹结构剩余强度准则提供试验依据。     

基于频域分析的ROSAR成像算法

在现有的ROSAR(Synthetic Aperture Radar with Rotating antennas)成像算法中,基于斜距泰勒级数展开的算法存在方位向失配问题,时域相关卷积算法不能快速校正距离弯曲.频域ROSAR成像算法采用驻相点原理,直接对ROSAR回波信号进行二维频域变换,保留回波信号的频谱特征,进而构造相应的频域去耦函数和频域匹配函数,实现频域距离弯曲校正和目标场景重构.仿真结果表明,该算法能够快速校正距离弯曲及有效克服方位向失配问题.