Preliminary Study on the Translunar Halo Orbits of the Real Earth–Moon System

The computation of translunar Halo orbits of the real Earth–Moon system (REMS) has been an open problem for a long time, but now, it is possible to compute Halo orbits of the REMS in a systematic way. In this paper, we describe the method used for the numerical computation of Halo orbits for a time span longer than 41 years. Halo orbits of the REMS are computed from quasi-periodic Halo orbits of the quasi-bicircular problem (QBCP). The QBCP is a model for the dynamics of a spacecraft in the Earth–Moon–Sun system. It is a Hamiltonian system with three degrees of freedom and depending periodically on time. In this model, Earth, Moon and Sun are moving in a self-consistent motion close to bicircular. The computed Halo orbits of the REMS are compared with the family of Halo orbits of the QBCP. The results show that the QBCP is a good model to understand the main features of the Halo family of the REMS.     

Reduced Hamiltonian formalism for general-relativistic adiabatic fluids and applications

For the dynamics of general-relativistic adiabatic fluids a reduced Hamiltonian formalism is presented. For slowly moving fluids an approximation scheme is defined. The first steps of the scheme are worked out explicitly. Radiation damping and emission, and backscattering are discussed. The usefulness of the formalism for numerical relativity is pointed out.     

西安东部夜间异常增温原因及其数值模式预报订正

利用陕西省气象监测站观测资料、NCEP/NCAR和ERA5全球再分析资料,对2019年12月10日凌晨西安东部一次夜间温度异常跃增过程进行深入分析.结果表明:①此次夜间增温过程发展迅速、局地性强、预报难度大.②500 hPa内蒙东部冷槽底后部干燥的西北气流和850 hPa干暖气团有利于产生大气下沉绝热增温.西安地区近地...     

湿位涡方程及其应用

本文在湿绝热、无摩擦条件下，推导了湿位涡方程及其近似表达式。然后通过尺度分析得到了大尺度条件下湿位涡守恒的性质，其形式与干位涡一样。由于考虑了水汽的作用，使用它较干位涡更为方便。最后，我们把湿位涡用于江南岭北3 月有无连阴雨的分析，其结果与预报员经验是一致的。     

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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Adiabatic invariants for the nonconservative Kepler's problem

This paper considers adiabatic invariants for the classical Kepler problem with resisting forces. The analysis is based on the theory of integrating factors and theory of adiabatic invariants in the Krylov-Bogoliubov-Mitropolski variables. The adiabatic invariants are series with respect to a small parameter. Also, for every particular case of nonconservative forces, it is shown that, with a complete set of adiabatic invariants, an approximate solution of the problem can be obtained. Four problems are analyzed in detail where approximate solutions are compared with numerical.     

用不变矩从机载激光扫描测高点云数据中重建规则房屋

介绍了不变矩的概念，结合实例，基于机载激光扫描测高的三雏点云数据，用不变矩实现了规则房屋的模型重建。对不变矩重建房屋模型的精度进行了讨论和分析．得出了一些有益的结论。     

小波分析在重力界面反演中的应用

基于Parker-Oldenburg反演方法，分析了低通滤波器B（K）的不同阈值对位场分离的影响。分别采用小波变换和低通滤波对青藏高原地区布格重力异常进行了位场分解和莫霍面反演，并将反演结果与地震资料作比较。结果表明，在重力位场分解中小波多尺度分解可以代替低通滤波器B（K），避免了闻值的选取。