Photometric Follow-up Transit (Primary Eclipse) Observations of WASP-43 b and TrES-3b and A Study on Their Transit Timing Variations     

Sun Zhao  Ji Jiang-hui  Dong Yao 《Chinese Astronomy and Astrophysics》2018,42(1):101-128

Two photometric follow-up transit (primary eclipse) observations on WASP-43 b and four observations on TrES-3 b are performed using the Xuyi Near-Earth Object Survey Telescope. After differential photometry and light curve analysis, the physical parameters of the two systems are obtained and are in good match with the literature. Combining with transit data from a lot of literature, the residuals (O ? C) of transit observations of both systems are fitted with the linear and quadratic functions. With the linear fitting, the periods and transit timing variations (TTVs) of the planets are obtained, and no obvious periodic TTV signal is found in both systems after an analysis. The maximum mass of a perturbing planet located at the 1:2 mean motion resonance (MMR) for WASP-43 b and TrES-3 b is estimated to be 1.826 and 1.504 Earth mass, respectively. By quadratic fitting, it is confirmed that WASP-43 b may have a long-term TTV which means an orbital decay. The decay rate is shown to be P? = (?0.005248 ± 0.001714) s·yr^?1, and compared with the previous results. Based on this, the lower limit of the stellar tidal quality parameter of WASP-43 is calculated to be ${Q^{\prime }}_{*}\ge 1.5\times {10}^5$, and the remaining lifetimes of the planets are presented for the different ${Q^{\prime }}_{*}$ values of the two systems, correspondingly.  相似文献   

Low-energy Lunar Trajectories with Lunar Flybystwo     

Wei Bing-wei  Li Yin-shan 《Chinese Astronomy and Astrophysics》2018,42(4):575-593

The low-energy lunar trajectories with lunar flybys are investigated based on the Sun-Earth-Moon bicircular problem (BCP). The characteristics of the distribution of trajectories in the phase space are summarized. Using the invariant manifolds in the BCP system, the low-energy lunar trajectories with lunar flybys are sought. Then, take time as an augmented dimension in the phase space of a nonautonomous system, we present the state space map and reveal the distribution of these lunar trajectories in the phase space. Consequently, we find that the low-energy lunar trajectories exist as families, and that the every moment in the Sun-Earth-Moon synodic period can be the departure date. Finally, we analyse the velocity increment, transfer duration, and system energy for the different trajectory families, and obtain the velocity-impulse optimal family and the transfer-duration optimal family, respectively.  相似文献   

略论海洋测高卫星GPS厘米级定轨的实施基础          下载免费PDF全文

刘基余 《海洋测绘》2010,30(6):1-4

基于对多种飞机的机载GPS测量实践,认为我国HY-2海洋二号卫星实现厘米级精度的星载GPS定轨测量的基础是:选择适合天线,捕获多颗在视GPS卫星;注重天线安装位置,减弱多路径效应影响;选择适合GPS信号接收机,确保星载GPS测量数据优质。  相似文献   

GPS卫星原子钟频率稳定度表征方法分析   总被引：1，自引：0，他引：1  

冯遂亮  宋力杰 《全球定位系统》2009,34(1):19-23

原子钟频率稳定度的表征通常在时域和频域进行,而对于“尺度域”小波方差表征方法的分析研究较少。对该方法进行系统归纳总结的基础上,给出时域尺度域两类不同表征方法的实用计算公式及其置信度计算方法,通过对各种方差特性的比较分析,指出其适用范围。分析表明：时域系列方差计算简单、直接,各具特点,可以满足不同的实际需要;尺度域的小波方差是一种具有独特优越性的新方法,但可以达到时域表征方法的效果,适用于进行原子钟频率稳定度的估计。  相似文献   

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贺凯飞  徐天河 《大地测量与地球动力学》2009,29(6):109-112

?????GEO????????????????????????????????????Kalman???????GEO?????????????????????????????????????η????????????????????????????????????????????????????????????????????????????????????з?????????????????????????????????????????Kalman???????????н????????????????к???????????????????????,????????????????Kalman????????????????????????????,???????Kalman???????????????????????????????????????????Kalman?????????????????????GEO?????????????  相似文献   

编队卫星InSAR系统的相位同步分析   总被引：1，自引：0，他引：1  

汤晓涛  楼良盛  刘志铭 《地球信息科学学报》2008,10(6):798-801

编队卫星InSAR系统属多基雷达系统,依靠编队卫星构型形成干涉所需的基线。一发多收工作模式下的编队卫星InSAR高程测量系统,协同工作的雷达间必须建立时间同步、相位同步和空间同步,其同步精度将影响InSAR系统的功能与性能。三大同步中,相位同步误差直接影响SAR复影像的相位误差,从而影响系统的高程测量精度。本文根据编队卫星条件下SAR成像的要求,对相位同步的要求进行了分析,并给出了由于相位不同步所引起的相位误差对InSAR高程测量精度影响。分析结果表明,编队卫星InSAR系统对于相位同步的要求包含两个方面:一是为保证被动雷达能够对回波实现相参成像,在整个合成孔径时间内,主动和被动两个雷达在载波相位上必须保持确定和可知的关系,且其差值随系统距离向分辨率的不同必须限定在一定范围内;二是在整个干涉数据的录取时间里,主动和被动两个雷达载波相位同步误差不能超过高程测量的精度要求所允许的误差。  相似文献   

Impact craters on small icy bodies such as icy satellites and comet nuclei     

M. J. Burchell  E. Johnson 《Monthly notices of the Royal Astronomical Society》2005,360(2):769-781

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On one special case of parametric resonance in problems of celestial mechanics     

A. P. Markeev 《Astronomy Letters》2005,31(5):350-356

We consider a periodic (in time) linear Hamiltonian system that depends on a small parameter. At a zero value of this parameter, the matrix of the system is constant, has two identical pairs of purely imaginary roots, and is not reducible to diagonal form. Therefore, the unperturbed system is unstable. We propose an algorithm for determining the boundaries of the instability regions for the system at nonzero values of the small parameter. This algorithm was used to analyze the stability of triangular libration points in the elliptical restricted three-body problem and in the stability problem in one special case of stationary rotation of a satellite relative to the center of mass.  相似文献   

The impact of the new Earth gravity models on the measurement of the Lense–Thirring effect with a new satellite     

Lorenzo Iorio   《New Astronomy》2005,10(8):616-635

In this paper we investigate the opportunities offered by the new Earth gravity models from the dedicated CHAMP and, especially, GRACE missions to the project of measuring the general relativistic Lense–Thirring effect with a new Earth’s artificial satellite. It turns out that it would be possible to abandon the stringent, and expensive, requirements on the orbital geometry of the originally prosed LARES mission (same semimajor axis a = 12,270 km of the existing LAGEOS and inclination i = 70°) by inserting the new spacecraft in a relatively low, and cheaper, orbit (a = 7500–8000 km, i  70°) and suitably combining its node Ω with those of LAGEOS and LAGEOS II in order to cancel out the first two even zonal harmonic coefficients of the multipolar expansion of the terrestrial gravitational potential J₂, J₄ along with their temporal variations , . The total systematic error due to the mismodelling in the remaining even zonal harmonics would amount to 1% and would be insensitive to departures of the inclination from the originally proposed value of many degrees. No semisecular long-period perturbations would be introduced because the period of the node, which is also the period of the solar K₁ tidal perturbation, would amount to 10² days. Since the coefficient of the node of the new satellite would be smaller than 0.1 for such low altitudes, the impact of the non-gravitational perturbations of it on the proposed combination would be negligible. Then, a particular financial and technological effort for suitably building the satellite in order to minimize the non-conservative accelerations would be unnecessary.  相似文献   

Methods for computing giant planet formation and evolution     

O. G. Benvenuto †  A. Brunini ‡ 《Monthly notices of the Royal Astronomical Society》2005,356(4):1383-1395

We present a numerical code for computing all stages of the formation and evolution of giant planets in the framework of the core instability mechanism. This code is a non-trivial adaption of the stellar binary evolution code and is based on a standard Henyey technique. To investigate the performance of this code we applied it to the computation of the formation and evolution of a Jupiter mass object from a half Earth core mass to ages in excess of the age of the Universe.
We also present a new smoothed linear interpolation algorithm devised especially for the purpose of circumventing some problems found when some physical data (e.g. opacities, equation of state, etc.) are introduced into an implicit algorithm like the one employed in this work.  相似文献