Effect of perturbations on the non linear stability of triangular points in the restricted three-body problem with variable mass

The effect of small perturbations ε and ε ^′ in the Coriolis and the centrifugal forces, respectively on the nonlinear stability of the triangular points in the restricted three-body problem with variable mass has been studied. It is found that, in the nonlinear sense, the triangular points are stable for all mass ratios in the range of linear stability except for three mass ratios, which depend upon ε, ε ^′ and β, the constant due to the variation in mass governed by Jeans’ law.     

Artificial halo orbits for low-thrust propulsion spacecraft

We consider periodic halo orbits about artificial equilibrium points (AEP) near to the Lagrange points L ₁ and L ₂ in the circular restricted three body problem, where the third body is a low-thrust propulsion spacecraft in the Sun–Earth system. Although such halo orbits about artificial equilibrium points can be generated using a solar sail, there are points inside L ₁ and beyond L ₂ where a solar sail cannot be placed, so low-thrust, such as solar electric propulsion, is the only option to generate artificial halo orbits around points inaccessible to a solar sail. Analytical and numerical halo orbits for such low-thrust propulsion systems are obtained by using the Lindstedt Poincaré and differential corrector method respectively. Both the period and minimum amplitude of halo orbits about artificial equilibrium points inside L ₁ decreases with an increase in low-thrust acceleration. The halo orbits about artificial equilibrium points beyond L ₂ in contrast show an increase in period with an increase in low-thrust acceleration. However, the minimum amplitude first increases and then decreases after the thrust acceleration exceeds 0.415 mm/s². Using a continuation method, we also find stable artificial halo orbits which can be sustained for long integration times and require a reasonably small low-thrust acceleration 0.0593 mm/s².     

Reconstruction of the Cenozoic deformation of the Bohai Bay Basin,North China

A well‐constrained plate deformation model may lead to an improved understanding of sedimentary basin formation and the connection between subduction history and over‐riding plate deformation. Building quantitative models of basin kinematics and deformation remains challenging often due to the lack of comprehensive constraints. The Bohai Bay Basin (BBB) is an important manifestation of the destruction of the North China Craton, and records the plate kinematic history of East Asia during the Cenozoic. Although a number of interpretations of the formation of the BBB have been proposed, few quantitative basin reconstruction models have been built to test and refine previous ideas. Here, we developed a quantitative deformation reconstruction of the BBB constrained with balanced cross‐sections and structural, stratigraphic and depositional age data. Our reconstruction suggests that the basin formation process was composed of three main stages: Paleocene‐early Eocene (65–42 Ma) extension initiation, middle Eocene‐early Oligocene (42–32.8 Ma) extension climax and post‐Oligocene (32.8–0 Ma) post‐extensional subsidence. The deformation of the BBB is spatially heterogeneous, and its velocity directions rotated clockwise during the basin formation process. The reconstruction supports the interpretation that the BBB formed via strike‐slip faulting and orthogonal extension and that the basin is classified as a composite extensional‐transtensional basin. We argue that the clockwise rotation of the basin velocity field was driven by the counter‐clockwise rotation in the direction of Pacific Plate subduction. The kinematics of the BBB imply that the Pacific Plate may have been sufficiently coupled to the over‐riding East Asian Plate during the critical period of Pacific Plate reorganization. The new reconstruction provides a quantitative basis for studies of deformation processes not only in the vicinity of the BBB, but also more broadly throughout East Asia.     

基于直线间几何属性特征相似性约束的组直线匹配算法

当影像中存在多个相同或相近的直线特征时,仅利用单直线特征间的相似性进行匹配容易导致算法失效,因此本文提出基于直线间几何属性特征相似性约束的组直线匹配算法。该算法利用直线间的拓扑关系分别对2幅影像上提取的直线进行编组得到特征直线组,并将其作为匹配基元;然后利用核线约束确定候选同名直线组的搜索范围,精简了候选直线组的数量;依据直线间几何属性特征向量的仿射不变性建立直线组的匹配关系,将仿射不变量交比作为基础几何不变性测度,并延伸设计仿射相似度参数,计算出目标直线组与每个候选直线组的仿射相似度或一般相似度,确定2种相似度下总体相似度值最大的特征直线组为其同名直线组,最后将同名直线组分裂为2对同名单直线,对分裂后的结果进行整合可以显著降低冗余匹配,得到“一对一”的匹配单直线。为了验证算法的可靠性,实验选取网上公开的5组典型近景影像进行测试,通过与其他匹配算法的对比分析,结果表明该算法应对影像间存在的视角、旋转和尺度变换等复杂条件均取得了较高的匹配精度,匹配正确率最高有14.5%的提升,且阈值的选择对匹配结果影响微弱,验证了基于直线间几何属性特征相似性约束的组直线算法鲁棒性和匹配稳定性较强。     

多视点相机联合标定及改进的PMVS重建方法

提出一种能够在强约束条件下快速进行相机标定的方法。通过相机间6个相互独立的约束,充分利用系统的几何条件,确定相邻立体相机的固有关系;再以共线方程为基础推导强约束条件下的平差模型,并应用于自检校光束法平差,从而实现多相机系统的快速标定;最后利用改进的PMVS三维重建方法开展标定后系统的人体三维重建。实验表明,通过加入强约束条件,增加平差的多余观测数,提高了标定精度和鲁棒性,对三维重建的精度亦有较大提高,并且该方法可推广到多个相机组成的多相机立体量测系统的标定中。     

一种加快BDS精密单点定位初始化的方法

由于BDS卫星的星座特性及卫星的轨道和钟差的精度影响,使得传统消电离层组合精密单点定位(PPP)的初始化时间较长。针对上述问题,文中对附加电离层约束的非组合精密单点定位算法进行研究。首先介绍非组合PPP算法,分析其与传统PPP的差异;其次分别利用CODE电离层格网产品,以反距离加权算法计算的站星电离层延迟、低阶球谐函数建立的区域电离层产品等作为先验信息对非组合PPP进行约束。通过MGEX观测网实测数据静态和仿动态计算表明,相比传统消电离层组合PPP,附加电离层约束的非组合PPP能够有效缩短初始化时间,同时能够获得高精度的定位结果。     

基于Android的控制点手持维护系统的设计与实现

针对传统的控制点管理方法无法解决信息量匮乏、信息现势性不足、不便于野外操作等问题,提出了一种新的基于Android的控制点手持管理方法。采用控制点信息建模技术和移动数据库接口技术,实现了对控制点信息的实时更新;采用网络地图服务集成技术,实现了对控制点信息的深度挖掘以及便于野外操作。通过基于Android的控制点手持维护系统的开发表明:结合Android终端与网络地图服务,可以避免传统方法的不足,更加有效的进行控制点的管理与维护。     

时空约束下的沙化土地遥感提取方法研究

针对辽西北中轻度沙化土地的区域特点和特殊性,通过分析其沙化土地的光谱特征、空间分布及时间变迁特征,研究了一种时空约束下的多光谱遥感影像沙化土地识别方法。在对沙化土地进行光谱特征分析的基础上,加入时-空分布特征进行约束修正,有效提高了沙化土地监测的精度和效率。     

高分辨率遥感影像主干道路提取的感知编组方法

针对高分辨率遥感影像的道路提取受"同物异谱、同谱异物"干扰的问题,该文提出一种基于感知编组的高分辨率遥感影像主干道路自动提取方法:首先,使用Line Segment Detector算法提取影像中直线段信息。然后,利用高分辨率遥感影像上的道路几何特征对直线段进行感知编组;最后,经过长度约束得到道路信息。使用两景影像进行了主干道路提取实验。实验结果表明,两个实验中主干道路提取的完整率、正确率和检测质量都在96%以上。     

基于三维激光扫描数据的建筑物三维建模

给出基于三维激光扫描测量仪所获得的点云数据来实现建筑物三维建模的方法。文中介绍了三维激光扫描测量仪的系统组成与工作原理,给出对点云数据处理的过程和方法,阐述建筑物三维建模的方法,并用实例介绍整体方法的实现过程和效果。