近地航天器量子导航定位卡尔曼滤波算法研究

针对近地航天器量子导航定位系统,为了进一步提高其定位精度,利用滤波技术将QPS测量值结合航天器的运动模型进行状态量的滤波估计.给出了基于基线干涉原理的量子定位系统观测方程和以二体运动为主的航天器轨道运动模型,在此基础上详细推导了扩展卡尔曼滤波处理过程,并针对该模型进行了仿真.仿真结果表明,基于EKF的量子导航定位精度有明显提高.     

一种基于激光捷联惯组的定瞄一体化系统设计

针对武器系统任意点随机发射和“ 停下即打” 目标的需求, 提出了一种基 于激光捷联惯组的定瞄一体化系统设计方案。系统由以激光捷联惯组为核心的车载定位 导航单元和以光管为核心的光学传递单元组成。由里程计、高程计、电子地图及卫星系 统辅助激光捷联惯组实现较高精度的定位导航功能。通过与车载定位导航单元刚性固联 的光学传递单元,采用光学传递方式实现与外部设备的瞄准,瞄准结果通过车载定位导 航单元完成。系统首次将定位瞄准实现一体化集成,在不损失水平瞄准精度的情况下, 降低了对瞄准环境的要求,达到预期效果。     

Inhibitory effect of simulated microgravity on differentiating preosteoblasts

The bone loss induced by microgravity is partly due to the decrease of mature osteoblasts. In the present study, we employed the random positioning machine (RPM) to simulate microgravity and investigated the acute effects of simulated microgravity on the differentiation of 2T3 preosteoblasts. Following 7 days’ culture under normal (1 g) condition, cells were exposed to simulated microgravity for 24 h. The results showed that 24 h treatment of simulated microgravity significantly decreased alkaline phosphatase (ALP) activity without changing the cell morphology. In addition, the mRNA expressions of osteogenic genes, including runt-related gene 2 (Runx2), osterix, osteocalcin (OC), type I collagen (Col I) and bone morphogenetic protein (BMP), were dramatically downregulated. Moreover, western blot analysis of total extracellular signal-regulated kinase (Erk) and phosphorylated Erk (p-Erk) indicated that p-Erk level, which represents the Erk activation status, was increased. Taken together, our results suggested that acute exposure to simulated microgravity inhibited osteoblast differentiation through modulating the expression of osteogenic genes and the Erk activity. These findings provide new insight for bone loss due to microgravity and unloading.     

GLONASS-based precise point positioning and performance analysis

Current precise point positioning (PPP) techniques are mainly based on GPS which has been extensively investigated. With the increase of available GLONASS satellites during its revitalization, GLONASS observations were increasingly integrated into GPS-based PPP. Now that GLONASS has reached its full constellation, there will be a wide interest in PPP systems based on only GLONASS since it provides a PPP implementation independent of GPS. An investigation of GLONASS-based PPP will also help the development of GPS and GLONASS combined PPP techniques for improved precision and reliability. This paper presents an observation model for GLONASS-based PPP in which the GLONASS hardware delay biases are addressed. In view of frequently changed frequency channel number (FCN) for GLONASS satellites, an algorithm has been developed to compute the FCN for GLONASS satellites using code and phase observations, which avoids the need to provide the GLONASS frequency channel information during data processing. The observation residuals from GLONASS-based PPP are analyzed and compared to those from GPS-based PPP. The performance of GLONASS-based PPP is assessed using data from 15 globally distributed stations.     

GPS载波相位时间传递软件的实现

研究了基于精密单点定位原理的GPS载波相位时间传递方法的数学模型和数据处理方法,设计了相应的程序流程,并基于Visual C++和Fortran混合编程的方式编写了相应的计算程序GPSCPTT V1.0。采用实际观测数据进行实验验证,结果表明,软件可以实现高精度的时间传递。     

基于STK的导航星模拟及天文定位选星算法研究

导航星优选是研究天文定位导航的前提。本文结合导航恒星选星对天文定位的影响,研究提出了基于STK软件的导航星模拟方法,并针对空天飞行器对天文观测时的条件约束,结合天文导航定位对导航星的要求,构建了适合不同飞行航迹的导航星库。基于所设计的导航星库,以空天飞行器为应用对象,结合其在轨段飞行轨迹参数,基于STK软件进行了天文导航定位仿真研究。在所设计的飞行器飞行航迹参数及可见星信息条件下,针对空天飞行器长航迹飞行运动特点,设计了3种不同的天文定位观测选星方案,并研究了不同选星方案下的天文导航定位性能。最后通过仿真验证表明所提出的导航星模拟和选星方法能有效满足空天飞行器对天文导航定位的要求。     

基于Windows系统环境下的精确定时过程实现

首先阐述Windows系统环境下的消息处理机制；然后对Windows下几种常用精确定时器进行比较；最后设计一种基于多线程技术的高精度定时器。通过实际测试，验证了该定时器的高精度性能，很好地实现了以毫秒级定时的通信任务。     

精密测量中等分定位概念的探讨

针对任意实际路程,研究了等分和定位诸多实际需要的技术和理论,阐述了以等分为手段,以定位为目的的等分定位概念。     

直线电机在划片机中的应用

介绍了直线电机在划片机中的应用,结果表明,直线电机在高精度定位和进给方面,性能优异。     

利用GPS进行航天器姿态确定的EKF方法

姿态确定是ＧＰＳ在航天器上应用的一个重要方面。采用广义卡尔曼滤波（ＥＫＦ）方法利用ＧＰＳ进行航天器姿态确定，建立了ＧＰＳ载波相位观测和航天器姿态运动的线性误差方程，并进行了仿真计算。