Self-alignment of full skewed RSINS：observability analysis and full-observable Kalman filter

Traditional orthogonal strapdown inertial navigation sys-tem （SINS） cannot achieve satisfactory self-alignment accuracy in the stationary base： taking more than 5 minutes and al the iner-tial sensors biases cannot get ful observability except the up-axis accelerometer. However, the ful skewed redundant SINS （RSINS） can not only enhance the reliability of the system, but also improve the accuracy of the system, such as the initial alignment. Firstly, the observability of the system state includes attitude errors and al the inertial sensors biases are analyzed with the global perspective method： any three gyroscopes and three accelerometers can be assembled into an independent subordinate SINS （sub-SINS）;the system state can be uniquely confirmed by the coupling connec-tions of al the sub-SINSs;the attitude errors and random constant biases of al the inertial sensors are observable. However, the ran-dom noises of the inertial sensors are not taken into account in the above analyzing process. Secondly, the ful-observable Kalman filter which can be applied to the actual RSINS containing random noises is established; the system state includes the position, ve-locity, attitude errors of al the sub-SINSs and the random constant biases of the redundant inertial sensors. At last, the initial self-alignment process of a typical four-redundancy ful skewed RSINS is simulated： the horizontal attitudes （pitch, rol ） errors and yaw error can be exactly evaluated within 80 s and 100 s respectively, while the random constant biases of gyroscopes and accelero-meters can be precisely evaluated within 120 s. For the ful skewed RSINS, the self-alignment accuracy is greatly improved, mean-while the self-alignment time is widely shortened.     

两时间尺度的捷联速度算法研究

根据奇异摄动理论分析具有小参数的捷联惯导系统方程,在两时间尺度上对系统状态方程进行了降阶简化处理,设计捷联算法.在内回路推力速度矢量计算中,应用一种新的划船补偿算法补偿比力转换过程中载体姿态变化产生的速度误差.在外回路中进行重力地速计算,完成导航坐标系上速度的更新.仿真结果表明:新算法精度与Savage四子样算法近似,计算量小.     

MEMS磁场传感器的设计及测试

以U型梁为主要结构设计了一种新型的洛伦兹力驱动的磁场传感器,检测在磁场中作切割磁力线运动的金属线上的感生电压,实现磁场测量.首先介绍了传感器的工作原理,并用振动理论对传感器的受力及响应进行了分析,接着用有限元软件建立结构模型并对其振动模态和频率进行了仿真.该MEMS磁场传感器采用标准的CMOS工艺加上后处理来实现.最后...     

大型高功率激光装置下装系统的碰撞检测

分析了大型高功率激光装置在线可替换单元装校过程的特殊性,建立了基于区域划分的下装系统的方向包围盒,在包围盒的计算中引入闵可夫斯基和的概念,并在其基础上对分离轴的选择进行优化组合,结合碰撞的局部性原理,构建了一种动态的OBB(Oriented Bounding Box)层次树检测方法,经过中国大型高功率激光装置下装系统的装校仿真实践,结果表明这种划分区域的连续检测方法高效可靠。     

Improved acetone sensing properties of flat sensors based on Co-SnO2 composite nanofibers

Co-SnO2 composite nanofibers were synthesized by an electrospinning method and characterized by X-ray diffraction, field emission scanning electron microscopy, and transmission electron microscopy. Gas sensors were fabricated by spinning these nanofibers onto flat ceramic substrates, which had signal electrodes and heaters on their top and bottom surfaces, respectively. Compared with sensors loaded with pure SnO2 nanofibers, the Co-SnO2 nanofiber sensors exhibited improved acetone sensing properties with high selectivity and rapid response and recovery times. The response was 33 when the sensors were exposed to 100 μL/L acetone at 330°C, and the corresponding response with 100 μL/L of ethanol was only 6. The response and recovery times to acetone were about 5 and 8 s, respectively. These results indicate Co-SnO2 composite nanofibers are good candidates for fabrication of high performance acetone sensors for practical application.     

某型末制导炮弹惯导陀螺动力学分析与仿真

目前国内外学者将惯导陀螺连同末制导炮弹弹体视作单刚体来研究,对于惯导陀螺内外框摆动角的确定是通过弹体坐标系、惯导陀螺坐标系和地面坐标系之间的转换关系推导出来的,并不能直接反应惯导陀螺内外框摆动的动力学规律.为了揭示惯导陀螺内外框摆动角变化的内在规律,得到多刚体条件下末制导炮弹角运动模型,首先进行基本假设、建立坐标系,其...     

基于MEMS的压电厚膜谐振梁能量收集器的研究

在谐振梁能量收集器中PZT膜材料的制备起着至关重要的作用,复合结构的锆钛酸铅(PZT)厚膜采用溶胶-凝胶方法旋涂在硅基的Au/Cr/SiO2/Si结构衬底的制备方法,主要因为溶胶-凝胶制备方法简单,成本低适合于集成制作.改进PZT组分和和0-3混合法及复合结构的Au/Cr/SiO2/Si衬底,使制备的PZT厚膜避免了厚...     

基于多尺度光流融合特征点视觉-惯性SLAM方法

为提高视觉-惯性导航系统在弱纹理环境下的鲁棒性和精度,结合特征点法精度高和光流法速度快的特点以及惯性信息,提出一种多尺度均匀化光流融合特征点法的视觉-惯性同时定位与地图(simultaneous localization and mapping, SLAM)构建方法。首先,改进快速特征点提取和描述(oriented fast and rotated brief, ORB)特征提取过程,采用多尺度网格化的方法提取ORB特征点并利用四叉树均匀分配特征点,提高特征分布离散性。其次,在帧间采用LK(Lucas and Kanade)光流法追踪特征点进行帧间的数据关联,在关键帧对特征点进行描述子的计算和匹配从而实现关键帧间的数据关联,保证算法速度的同时提高定位精度和鲁棒性。最后,基于光流法建立的数据关联得到的初始位姿为后端优化提供初始值,整合ORB特征点重投影误差、惯性测量单元(inertial measurement unit, IMU)预积分误差以及滑动窗口先验误差构建最小化目标函数采用滑动窗口非线性优化进行求解。实验表明,所提方法相比单目视觉惯性系统具有更高的定位精度和鲁棒性,定位精度平均...     

舰载飞机着舰撞击载荷实测技术研究

针对国内飞机起落架载荷测量中普遍存在的静标动测问题,从理论和机理上分析了静标定的应变法实测动态载荷存在问题的原因。同时,考虑到舰载飞机因定点着舰方式遭受严重的动态载荷,重点研究了舰载飞机着舰撞击载荷的静标动测问题。通过动态落震试验模拟飞机着舰过程,根据测力平台的实测载荷分析,获取了应变法实测载荷精度受动态影响的程度,提出一种改进的惯性修正方法,即:通过落震试验数据辨识质量矩阵,通过辨识的质量矩阵和实测加速度修正应变法的实测载荷。试验结果表明,改进的惯性修正方法进一步提高了垂向载荷的测量精度,显著提高了航向和侧向载荷的实测精度。     

硅基微电感的研究

阐述了一种在硅杯表面采用浓硼扩散区与镀金属膜形成的欧姆接触电极作为内引线的硅基电感的新制造方法,提出了在硅杯背面用激光器打孔以减薄衬底厚度,从而使电感的Q值得到提高的一种方案,并应用目前普遍采用的电感模型,利用Ansys有限元软件中的电磁分析模块模拟了电感几何参数与磁感应强度、电感值的关系。结果表明,该方法具有制造工艺简单、与IC工艺相兼容的优点,有广泛的应用领域。