近百年中国、北半球和南半球气温内在结构比较（I）

气温气候资料是一个含有月、年、十年、百年等时间尺度的分形客体．大尺度上是冷暖之分,而每个冷（或暖）又分为较小尺度上的冷暖,形成层次结构．利用它的子波变换的尺度α－时间位置ｔ０表述,可以构造出分段线性一维映射动力系统,这个映射表征气候的层次结构,反映气候变化的突变点时间位置的规律和标度不变性．文中讨论了构造一维动力映射的基本原理,并以中国气温为例进行了验证．     

由GOCE引力梯度张量不变量确定卫星重力模型的半解析法

提出了利用半解析方法解算重力场与稳态海洋环流探测器(gravity field and steady-state ocean circulation explorer,GOCE)引力梯度张量不变量观测值来恢复全球卫星重力模型的方法,该方法比最小二乘方法效率高,同样可给出模型的验后方差。推导了半解析法快速解算引力梯度张量不变量的理论公式,给出了该方法利用卫星重力梯度观测数据快速求解重力场模型的基本步骤。利用89.5°倾角圆形严格重复轨道上的模拟梯度观测值验证了半解析方法用于张量不变量解算的理论严密性,并利用GOCE任务61 d 梯度仪坐标系(gradiometer reference frame,GRF)下无噪声和有噪声的I₂和V_zz模拟观测值进行了模型反演和结果分析。结果表明,利用I₂观测值求解模型的精度略优于仅用V_zz分量解算模型的精度。     

基于非全张量卫星重力梯度数据的张量不变量法

在非全张量卫星重力梯度观测数据的处理过程中,由于卫星姿态角误差、梯度观测数据误差和非全张量观测等原因,重力梯度值从卫星重力梯度仪系转换到地固系后,精度损失严重.本文研究了张量不变量法以解决上述问题.首先在重力梯度张量不变量线性化的基础上,建立了基于卫星轨道面的不变量观测模型,完整地推导了两类重力梯度张量不变量的球近似和顾及地球扁率影响的球面边值问题的求解公式.针对GOCE卫星任务非全张量观测数据类型,分析了张量不变量的计算误差;结果表明,重力梯度观测误差在不变量的计算中并没有被放大.最后运用广义轮胎调和分析方法进行了模拟试验,数值试验证明,在卫星姿态误差较大时,处理张量不变量比处理张量分量更具优势,并且张量不变量法能有效地解决非全张量观测的问题.     

Low Energy Transfer to the Moon

In 1991, the Japanese Hiten mission used a low energy transfer with a ballistic capture at the Moon which required less Vthan a standard Hohmann transfer. In this paper, we apply the dynamical systems techniques developed in our earlier work to reproduce systematically a Hiten-like mission. We approximate the Sun–Earth–Moon-spacecraft 4-body system as two 3-body systems. Using the invariant manifold structures of the Lagrange points of the 3-body systems, we are able to construct low energy transfer trajectories from the Earth which execute ballistic capture at the Moon. The techniques used in the design and construction of this trajectory may be applied in many situations.     

Introduction to an Invariant Quantity Method

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EJECTION–COLLISION ORBITS AND INVARIANT PUNCTURED TORI IN A RESTRICTED FOUR‐BODY PROBLEM

We study the motion of an infinitesimal mass point under the gravitational action of three mass points of masses μ, 1–2μ and μ moving under Newton's gravitational law in circular periodic orbits around their center of masses. The three point masses form at any time a collinear central configuration. The body of mass 1–2μ is located at the center of mass. The paper has two main goals. First, to prove the existence of four transversal ejection–collision orbits, and second to show the existence of an uncountable number of invariant punctured tori. Both results are for a given large value of the Jacobi constant and for an arbitrary value of the mass parameter 0<μ≤1/2. This revised version was published online in July 2006 with corrections to the Cover Date.     

Dynamics of a satellite orbiting a planet with an inhomogeneous gravitational field

We study the dynamics of a satellite (artificial or natural) orbiting an Earth-like planet at low altitude from an analytical point of view. The perturbation considered takes into account the gravity attraction of the planet and in particular it is caused by its inhomogeneous potential. We begin by truncating the equations of motion at second order, that is, incorporating the zonal and the tesseral harmonics up to order two. The system is formulated as an autonomous Hamiltonian and has three degrees of freedom. After three successive Lie transformations, the system is normalised with respect to two angular co-ordinates up to order five in a suitable small parameter given by the quotient between the angular velocity of the planet and the mean motion of the satellite. Our treatment is free of power expansions of the eccentricity and of truncated Fourier series in the anomalies. Once these transformations are performed, the truncated Hamiltonian defines a system of one degree of freedom which is rewritten as a function of two variables which generate a phase space which takes into account all of the symmetries of the problem. Next an analysis of the system is achieved obtaining up to six relative equilibria and three types of bifurcations. The connection with the original system is established concluding the existence of various families of invariant 3-tori of it, as well as quasiperiodic and periodic trajectories. This is achieved by using KAM theory techniques.     

孤立内波对过渡海域声场干涉结构的影响分析

南海北部陆坡海域是孤立内波的活跃区,孤立内波在该海域能够引起水体环境较强烈的水平不均匀性,从而影响声场干涉结构。将描述宽带声信号强度干涉条纹斜率的波导不变量视为一种分布,能更准确地分析声场的距离*频率干涉结构。本文研究了孤立内波环境下过渡海域声场的距离*频率干涉结构,依据实测孤立内波海洋环境,得到孤立内波环境下随距离变化的声速剖面,利用抛物方程方法仿真过渡海域声场干涉结构。在此基础上,利用拉东变换和傅里叶变换结合的谱值分离方法在低信噪比环境下提取波导不变量分布。分析表明孤立内波环境下过渡海域的声场类影区、类会聚区的波导不变量取值更丰富。     

Phase Equilibrium and Phase Diagram of the Ternary System(MgCl_2 + MgB_2O_4 + H_2O) at 288 and 298 K

正1 Introduction The brines with high concentrations of magnesium and boron resources are widely distributed in the Qaidam Basin of the Qinghai-Tibet plateau,China(ZhengTang,1988).Although some works on the ternary system