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1.
从月球的自由天平动,引力场和耗散等可以研究月球内部的结构和演化.本文从理论上估计了用激光测月资料推算月球自由天平动的精确度,根据四个激光测月台站的18年的观测资料计算了月球自由天平动的振幅和相位、月球转动惯量等,并初步得到了月球的内部结构和组成成分.  相似文献   

2.
本利用1970年1月至1987年12月的全球激光测月资料,确定了月球平黄径的长期加速度·/n的值为-25″.4±0″.1/cy^2。这一结果和用其它方法求得的·/n值符合得很好。利用激光测月解算·/n的内符精度随所用资料的时间跨度的增加而迅速提高。  相似文献   

3.
本文在视月球自由天平动为受迫天平动的附加运动之物理思想前提下,借助于雅可比行列式变换的数学手段,具体推导了激光测月理论时延τ。对月球自由天平动参数的偏导数,从而给出LLR法检测月球自由天平动的原理。  相似文献   

4.
本对激光测月资料分析中的相对论效应作了较系统的分析讨论,包括观测时刻的转换,TAI和 TDB两种时间尺度的换算、测站的地心坐标和反射器的月心坐标到太阳系质心框架下的瞬时空间坐标的转换以及引力时延改正等一系列问题。同时比较分析了目前我们算软件中的相对论模型,指出原模型必须作适当的改进才能和厘米级的观测精度相匹配。  相似文献   

5.
月球激光测距的新技术方法研究   总被引:1,自引:0,他引:1  
月球激光测距是国内外所瞩目的宏伟目标,代表着单光子探测技术的高峰。本论文的目的是探索提高激光测月回波光子数的新方法,进而增加激光测月成功的几率。其思路是源于一个新的想法:在激光测月过程中引入大气波前倾斜量实时补偿的技术。首先介绍激光测月的现状和其难度所在:回波光子数太少,基本上属于亚光子探测范畴。在现有技术条件下,本文对影响激光测月回波光子数的因素逐一进行分析讨论,提出应该把激光束截面能量分布和大气湍流效应包括进去。为此分析讨论了大气湍流和大气中光场的基本统计性质、激光束在大气中传输时所受大气湍流的影响以及大气湍流对激光测距的影响,得出大气湍流特别对激光测月有着明显影响的结论。在此基础上对传统的激光测距方程进行了修正,使其应用到激光测月时更符合真实的情况,从而指导补偿的进行。涉及到在激光测月中对受大气湍流而畸变的激光束进行补偿,本文抓住重点,通过分析看出对大气倾斜量的实时补偿是提高激光测月回波光子数的重要因素。结合激光测月以及云南天文台现有测距系统的实际情况,本文独创性地提出利用激光测月目标近旁一定大小区域的扩展面源探测与计算大气倾斜量,然后对激光测月中的激光束进行大气倾斜量实时补偿的新技术方法。在分析比较各种从低对比度扩展源中计算大气倾斜量的算法后,本文认为采用绝对差分法最佳。最后是具体的激光测月的新技术方案,同时对此方法的理论与技术进行了分析讨论,推导出新技术方法的理论依据、补偿效果、可行性与实用性。  相似文献   

6.
新版慧星轨道根数表发表1993年5月17日国际天文学联合会快报5792期报道,《音星轨道根数表》第8版已经在美国出版,厚102页,载有直到1993年4月的1392次普星出现期的相应轨道根数。这种数据表由国际天文学联合会的天文电报中心出版,从1972年...  相似文献   

7.
本文研究了1986-1988年美国喷气推进实验室、法国地球动力学中心和上海天文台用激光测月资料推算的UT1-UTC值,并与国际地球自转参数服务给出的UT1-UTC值作比较,得到各分析中心推算UT1-UTC值的内符和外符。  相似文献   

8.
本主要讨论了利用激光测月资料解算UT的两种方法:一种方法为仅仅解算世界时TU,另一种方法是同时求解UT和纬度变化△φ。经过实际计算和分析比较,结果表明:就目前的观测资料而言,只解UT的方案对解算UT值较有利。本着重讨论了在逐步回归解算中,自变量之间的相关性问题,这种情况下采用岭回归法解算,结果会有所改善。  相似文献   

9.
月球激光测距是国内外所瞩目的宏伟目标 ,代表着单光子探测技术的高峰。本论文的目的是探索提高激光测月回波光子数的新方法 ,进而增加激光测月成功的几率。其思路是源于一个新的想法 :在激光测月过程中引入大气波前倾斜量实时补偿的技术。首先介绍激光测月的现状和其难度所在 :回波光子数太少 ,基本上属于亚光子探测范畴。在现有技术条件下 ,本文对影响激光测月回波光子数的因素逐一进行分析讨论 ,提出应该把激光束截面能量分布和大气湍流效应包括进去。为此分析讨论了大气湍流和大气中光场的基本统计性质、激光束在大气中传输时所受大气湍流的影响以及大气湍流对激光测距的影响 ,得出大气湍流特别对激光测月有着明显影响的结论。在此基础上对传统的激光测距方程进行了修正 ,使其应用到激光测月时更符合真实的情况 ,从而指导补偿的进行。涉及到在激光测月中对受大气湍流而畸变的激光束进行补偿 ,本文抓住重点 ,通过分析看出对大气倾斜量的实时补偿是提高激光测月回波光子数的重要因素。结合激光测月以及云南天文台现有测距系统的实际情况 ,本文独创性地提出利用激光测月目标近旁一定大小区域的扩展面源探测与计算大气倾斜量 ,然后对激光测月中的激光束进行大气倾斜量实时补偿的新技术方法。在分析比较  相似文献   

10.
激光测月中的地球和月球参考架   总被引:2,自引:0,他引:2  
本讨论了激光测月 算地面台站坐标和月面反射器的月面坐标过程中初值的影响及迭代求解的稳定性问题。并指出影响地面台站坐标中地心经度分量的精度有两方面的原因,一是平差时采用的UT1值有误差,二是月球的赤经误差,后将引起地面台站产生一个沿经度方向的系统旋转,而这是所采用的月球星历表的误差所致。通过实例迭代运算表明, 测站坐标结果可以收敛到2cm左右,月面反射器在月面柱坐标中的σ和Z分量的结果可以稳定在10cm左右,而其λ分量目前只能达到米级。  相似文献   

11.
The multicollinearity among regression variables is a common phenomenon in the reduction of astronomical data. The phenomenon of multicollinearity and the diagnostic factors are introduced first. As a remedy, a new method, called adaptive ridge regression (ARR), which is an improved method of choosing the departure constant θ in ridge regression, is suggested and applied in a case that the Earth orientation parameters (EOP) are determined by lunar laser ranging (LLR). It is pointed out, via a diagnosis, the variance inflation factors (VIFs), that there exists serious multicollinearity among the regression variables. It is shown that the ARR method is effective in reducing the multicollinearity and makes the regression coefficients more stable than that of using ordinary least squares estimation (LS), especially when there is serious multicollinearity. This revised version was published online in July 2006 with corrections to the Cover Date.  相似文献   

12.
Reflectance Spectral Characteristics of Lunar Surface Materials   总被引:2,自引:0,他引:2  
Based on a comprehensive analysis of the mineral composition of major lunar rocks (highland anorthosite, lunar mare basalt and KREEP rock), we investigate the reflectance spectral characteristics of the lunar rock-forming minerals, including feldspar, pyroxene and olivine. The affecting factors, the variation of the intensity of solar radiation with wavelength and the reflectance spectra of the lunar rocks are studied. We also calculate the reflectivity of lunar mare basalt and highland anorthosite at 300 nm, 415 nm, 750 nm, 900 nm, 950 nm and 1000 nm. It is considered that the difference in composition between lunar mare basalt and highland anorthosite is so large that separate analyses are needed in the study of the reflectivity of lunar surface materials in the two regions covered by mare basalt and highland anorthosite, and especially in the region with high Th contents, which may be the KREEP-distributed region.  相似文献   

13.
A new method has been devised to determine the spherical harmonic coefficients of the lunar gravity field. This method consists of a two-step data reduction and estimation process. In the first step, a weighted least-squares empirical orbit determination scheme is applied to Doppler tracking data from lunar orbits to estimate longpperiod Kepler elements and rates. Each of the Kepler elements is represented by an independent function of time. The long-period perturbing effects of the Earth, Sun, and solar radiation are explicitly modeled in this scheme. Kepler element variations estimated by this empirical processor are then ascribed to the non-central lunar gravitation features. Doppler data are reduced in this manner for as many orbits as are available. In the second step, the Kepler element rates are used as input to a second least-squares processor that estimates lunar gravity coefficients using the long-period Lagrange perturbation equations.Pseudo Doppler data have been generated simulating two different lunar orbits. This analysis included the perturbing effects of the L1 lunar gravity field, the Earth, the Sun, and solar radiation pressure. Orbit determinations were performed on these data and long-period orbital elements obtained. The Kepler element rates from these solutions were used to recover L1 lunar gravity coefficients. Overall results of this controlled experiment show that lunar gravity coefficients can be accurately determined and that the method is dynamically consistent with long-period perturbation theory.  相似文献   

14.
基于对 2 0世纪中国大陆 7.0级以上大地震与月亮白赤交角的变化和太阳活动的研究结果 ,根据对未来 50a (年 )月亮白赤交角的值与目前太阳活动的形势 ,提出 2 1世纪中国大陆第一个大地震活动幕可能是 2 0 0 6或 2 0 0 7~ 2 0 1 5年  相似文献   

15.
The aim of this work is to combine the model of orbital and rotational motion of the Moon developed for DE430 with up-to-date astronomical, geodynamical, and geo- and selenophysical models. The parameters of the orbit and physical libration are determined in this work from lunar laser ranging (LLR) observations made at different observatories in 1970–2013. Parameters of other models are taken from solutions that were obtained independently from LLR. A new implementation of the DE430 lunar model, including the liquid core equations, was done within the EPM ephemeris. The postfit residuals of LLR observations make evident that the terrestrial models and solutions recommended by the IERS Conventions are compatible with the lunar theory. That includes: EGM2008 gravitational potential with conventional corrections and variations from solid and ocean tides; displacement of stations due to solid and ocean loading tides; and precession-nutation model. Usage of these models in the solution for LLR observations has allowed us to reduce the number of parameters to be fit. The fixed model of tidal variations of the geopotential has resulted in a lesser value of Moon’s extra eccentricity rate, as compared to the original DE430 model with two fit parameters. A mixed model of lunar gravitational potential was used, with some coefficients determined from LLR observations, and other taken from the GL660b solution obtained from the GRAIL spacecraft mission. Solutions obtain accurate positions for the ranging stations and the five retroreflectors. Station motion is derived for sites with long data spans. Dissipation is detected at the lunar fluid core-solid mantle boundary demonstrating that a fluid core is present. Tidal dissipation is strong at both Earth and Moon. Consequently, the lunar semimajor axis is expanding by 38.20 mm/yr, the tidal acceleration in mean longitude is \(-25.90 {{}^{\prime \prime }}/\mathrm{cy}^2\), and the eccentricity is increasing by \(1.48\times 10^{-11}\) each year.  相似文献   

16.
New Trends in the Development of the Lunar Physical Libration Theory   总被引:4,自引:0,他引:4  
A review of the modern state of the lunar libration theory is presented. A significant progress in the lunar investigation is achieved due to the simultaneous processing of results of the satellite Doppler tracing and of the lunar laser ranging. The data evidencing existence of a small iron core in the Moon are discussed. In this connection, the further development of the theory of rotation of the Moon presents the study of internal structure and dynamics of a lunar body. A model of a two-layer Moon can have a very advanced application to explain some observed phenomena and to be as a first approach in the modelling of internal processes determining the lunar rotation.  相似文献   

17.
Photoelectric observations have been carried out during maximum solar activity in order to investigate the variation of the brightness of the lunar surface with the solar cycle and to detect the possiblity of existing colour anomaly. The brightness data, using a wide-passband filter, do not show any evidence of variation with the solar cycle. No colour anomaly is found for the investigated lunar regions, and the doubt that has been felt by some investigators about the nonexistence of certain colour indices' variation with phase is not confirmed.  相似文献   

18.
Information about the structure of lunar interior and evolution could be obtained from measurements of lunar free librations, gravitational field, dissipation etc.. In this paper the precision of determining free librations with Lunar Laser Ranging (LLR) data are estimated. Using the observing data from four telescopes for eighteen years the amplitudes and phases of free librations, the moments of inertia ratio of The Moon were determined.  相似文献   

19.
环月飞行器精密定轨的模拟仿真   总被引:11,自引:2,他引:11  
胡小工  黄珹  黄勇 《天文学报》2005,46(2):186-195
以中国正在实施的探月计划“嫦娥1号”工程为背景,分析了在中国联合S波段(USB)测控网和甚长基线射电干涉(VLBI)跟踪网的现有空间分布、观测精度水平下的环月飞行器精密定轨.采用的方法是模拟仿真计算,即首先模拟观测数据,然后在计入各误差源的影响后进行求解,并对解算结果进行比较.模拟仿真的工具是美国宇航局哥达德飞行中心的空间数据分析软件系统GEODYN.环月飞行的主要误差源是月球重力场,为此首先讨论了目前精度最高的月球重力场模型JGL165P1的(形式)误差.在模拟了测距、测速以及VLBI的时延、时延率数据后,计入月球重力场的误差进行精密轨道确定.定轨时采用了减缩动力学(reduced dynamic)方法,即选用合适的经验加速度参数吸收重力场误差对定轨的影响.结果表明对于一个不将月球重力场作为主要科学目标的探月计划(如“嫦娥1号”),减缩动力学方法是一个简单、有效地提高环月飞行器定轨精度的方法.  相似文献   

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