关于学习效果的一个数学模型

本文对学习效果与学生素质、学习压力之间的关系进行了分析，用突变理论建立了一个数学模型。     

二重积分中值定理中间点的进一步讨论

众所周知,二重积分中值定理一般表述为：“设Ｄ为平面上有界闭区域,ｆ（ｘ,ｙ）在Ｄ上连续,ｇ（ｘ,ｙ）在Ｄ上可积且不变号,则至少存在一点（ζη）∈Ｄ,使得∫∫Ｄｆ（ｘ,ｙ）ｇ（ｘ,ｙ）ｄｘｄｙ＝ｆ（ζη）∫∫Ｄｇ（ｘ,ｙ）ｄｘｄｙ。”进一步证明了中间点（ζη）可选为Ｄ的内点,其结论与方法完全可推广到一般多重积分中值定理。     

直升机外挂飞行中的飘摆问题

主要研究直升机外挂飞行中，由于操纵方式或直升机的稳定特性及外挂形式等原因，使直升机产生飘摆，飘摆会影响任务的完成及飞行安全、从飘摆的机理出发，重点分析飘摆产生的基本条件及横向飘摆产生的原因，以及县挂点位置、吊索长度、外挂物形状等对直升机和外挂物耦合运动的影响。并给出对飘摆的处置方法和预防措施。为保证飞行安全提供理论基础和实际飞行经验。     

Feasibility study of autonomous orbit determination using only the crosslink range measurement for a combined navigation constellation

In order to expand the coverage area of satellite navigation systems, a combined navigation constellation which is formed by a global navigation constellation and a Lagrangian navigation constellation was studied. Only the crosslink range measurement was used to achieve long-term precise autonomous orbit determination for the combined navigation constellation, and the measurement model was derived. Simulations of 180 days based on the international global navigation satellite system(GNSS) service(IGS) ephemeris showed that the mentioned autonomous orbit determination method worked well in the Earth–Moon system. Statistical results were used to analyze the accuracy of autonomous orbit determination under the influences of different Lagrangian satellite constellations.     

地月系L1点的月球借力间接转移轨道设计

针对地月系L1点（LL1）的轨道转移问题,在平面圆型限制性三体问题模型下,提出了利用月球借力的间接转移设计方法.转移设计分为地月转移轨道段和月球至LL1流形段.首先,通过改变LL1点初始机动速度,逆向积分LL1点的拟流形,以寻找初始速度、月心会合坐标系下的轨道高度和相位角这三者之间的关系,确定月球—LL1流形段微分改正的初始条件.然后,借助地月系不同转移时间的霍曼转移轨道所对应的近月点高度和相位角的关系,获得使2段转移在近月点相拼接的地月转移轨道段.这种设计方法给出了一系列LL1点间接转移轨道,将此设计结果与其他文献中的转移设计方法进行比较,此间接转移轨道比低能量转移轨道节省时间,比直接转移轨道节约能量.     

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。     

一种结合深度学习的运动去模糊视觉SLAM方法

针对高动态环境下视觉同步定位与地图构建（Simultaneous Localization And Mapping,SLAM）系统的可靠性受运动模糊的限制,研究了一种基于生成对抗网络(Generative Adversarial Network,GAN)和AKAZE特征点的运动去模糊视觉SLAM方案。首先对因相机快速运动而产生的模糊图像进行AKAZE特征点的提取与检测,并根据特征点分布的丰富程度计算图像块权重,结合灰度图像的方差信息建立特征点与模糊程度之间的量化关系表;之后将达到模糊分数阈值的图像同步输入至改进GAN网络模型,该网络以端对端的形式恢复中心模糊帧的纹理信息,最后将输出的清晰图像重新进行位姿估计参与ORB-SLAM2后端优化过程。在公开数据集TUM上进行测试,对于受模糊影响较严重的数据集,方案可以明显降低相机轨迹估计的整体误差,同时维持较好的鲁棒性。     

基于遥感图像的无固定标志点卫星自主定轨

目前基于事先选取地面标志点的卫星自主导航可能会造成误匹配和漏匹配,并且不包含地标点的遥感图像也有可能存在导航信息.为了解决这两个问题,本文提出了一种不依赖事先标定地面标志点的自主导航方法,通过YOLOv3深度学习对获得的遥感图像进行目标识别缩小图像匹配区域,将识别后的目标区域进行图像匹配获得匹配特征点及其像平面坐标,最...     

基于特征点互信息预配准的医学图像配准技术

基于最大互信息的医学图像配准算法近几年来成为医学图像处理领域的热点。由局部极值导致的寻优困难是困扰该算法的核心问题,混合优化算法成功地解决了互信息函数的寻优问题,但延长了配准时间。文中研究了互信息函数峰值周围的局部极值特征,提出安全区域的概念。利用特征点互信息理论,并结合多灰度级和多分辨率策略,提出一种基于混合优化算法寻优和特征点互信息预配准的改进型算法。经过模拟数据和实际数据配准实验证明,该算法在保证了配准精度的同时,提高了配准的速度,稳健性更强,具有临床推广价值。