建立抵偿坐标系统解决长度变形的探讨

根据测量中长度变形的具体情况分析引起长度变形的因素,阐述了建立抵偿坐标系统解决长度变形的方法,主要有确定抵偿投影面高程和新椭球参数,将原坐标换算到抵偿坐标系等.进行了算例分析,并验证了该方法的正确性.     

A NEW ONE—DIMENSIONAL CHAOTIC MAP WITH INFINITE COLLAPSES

This letter presents a new one-dimensional chaotic map with infinite collapses. Theoretical analyses show that the map has complicated dynamical behavior and ideal distribution. The map can be applied in chaotic spreading spectrum communication and chaotic cipher.     

利用接收电视信号的多站系统进行目标定位以克服距离模糊

较短的不模糊距离是以电视信号为辐射源的双基地探测系统所面临的难题之一,本文深入研究了利用测量距离和的目标定位方法克服距离模糊的机理,提出了根据发射源的最大辐射距离,来确定最大不模糊可测椭球面的最优方法,指出了基线距离与最大不模糊可测空域的变化关系,对充分发挥辐射源的威力和选择最大不模糊可测空域提出了一条有效的途径.     

井眼测量误差椭球最小间距计算方法

随着丛式井和加密井在油田的广泛应用,对井眼防碰分析提出了更高的要求。井眼分离系数是防碰分析的一个常用指标,然而不同误差椭球分离距计算方法导致结果差异较大,为此提出测量误差椭球最小间距计算新方法,以更好地满足应用需要。在坐标变换及误差椭球计算基础上,推导了中心向量法误差椭球分离距计算公式,进而应用最优化理论求解了两误差椭球最小间距,并研究了快速求解策略,可精确、快速地计算井眼分离系数。算例分析表明,与其他计算方法相比,新方法能更好地指导井眼防碰风险评价工作,在丛式井设计和定向钻井中具有应用价值。     

单层椭球面网壳的参数化设计

根据椭球面网壳的特点,采用通用有限元软件ANSYS的APDL参数化语言,研制了两种类型的单层椭球面网壳,并实现了在给定几何参数:纵向跨度S1、横向跨度S2、矢高F、环向对称区域份数Kn、径向节点圈数Nx下,即可确定单层椭球面网壳的形式.通过设计实例表明,该参数化设计方式简单、高效、实用,为采用ANSYS软件对椭球面网壳的不同类型的设计及分析奠定了良好的基础.     

铌酸锂电光调制器的温度特性研究

采用折射率椭球基本理论和数值计算方法,分析了纵向和横向调制下,出射光光强随温度的变化趋势,以及在这过程中与晶体折射率、晶体热膨胀系数及晶体尺寸间的关系,并进行了相应的数值模拟。结果表明,纵向调制下出射光光强随温度的变化趋势只跟晶体折射率的变化有关;横向调制下出射光光强随温度的变化趋势不仅要受到晶体折射率的影响,还要受到晶体尺寸及其膨胀系数的影响,因此可以利用特殊尺寸的晶体来提高电光调制器的温度稳定性。     

基于FKICA-SIFT特征的合成孔径图像多尺度配准

针对合成孔径(SAR)图像的配准,提出一种基于仿射不变快速核独立成分分析-尺度不变特征变换(FKICA-SIFT)的多尺度配准方法.首先,根据特征点的Hessian矩阵构建仿射不变SIFT描述子.接着,利用FKICA提取该描述子的独立成分得到新的描述子FKICA-SIFT.然后,利用该描述子对Steerable滤波后的...     

基于三维环境下资源量估算及分级方法研究

分析了传统断面平均法矿量估算存在的优缺点,指出了利用三维矿业软件进行矿量估算的必要性。研究了三维地质矿量估算理论和基于块段模型及搜索椭球体的工程控制程度划分方法,并将该方法成功应用于某铜矿资源储量估值中。应用研究证明了利用该方法进行资源储量估算和分级的正确性和可行性。     

Halo orbit mission correction maneuvers using optimal control

This paper addresses the computation of the required trajectory correction maneuvers for a halo orbit space mission to compensate for the launch velocity errors introduced by inaccuracies of the launch vehicle. By combining dynamical systems theory with optimal control techniques, we are able to provide a compelling portrait of the complex landscape of the trajectory design space. This approach enables automation of the analysis to perform parametric studies that simply were not available to mission designers a few years ago, such as how the magnitude of the errors and the timing of the first trajectory correction maneuver affects the correction ΔV. The impetus for combining dynamical systems theory and optimal control in this problem arises from design issues for the Genesis Discovery Mission being developed for NASA by the Jet Propulsion Laboratory.     

Who needs QP for linear MPC anyway?

Conventional MPC uses quadratic programming (QP) to minimise, on-line, a cost over n linearly constrained control moves. However, stability constraints often require the use of large n thereby increasing the on-line computation, rendering the approach impracticable in the case of fast sampling. Here, we explore an alternative that requires a fraction of the computational cost (which increases only linearly with n), and propose an extension which, in all but a small class of models, matches to within a fraction of a percent point the performance of the optimal solution obtained through QP. The provocative title of the paper is intended to point out that the proposed approach offers a very attractive alternative to QP-based MPC.