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The Possible Signs of Hydrogen and Helium Accretion from Interstellar Medium on the Atmospheres of F-K Giants in the Local Region of the Galaxy 银河系局部区域F-K巨星大气中星际介质中氢和氦吸积的可能迹象
IF 0.5 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2021-09-01 DOI: 10.5140/jass.2021.38.3.175
A. Yushchenko, Seunghyun Kim, Yeuncheol Jeong, A. Demessinova, V. Yushchenko, D. Doikov, V. Gopka, K. S. Jeong, P. Rittipruk
The dependencies of the chemical element abundances in stellar atmospheres with respect to solar abundances on the second ionization potentials of the same elements were investigated using the published stellar abundance patterns for 1,149 G and K giants in the Local Region of the Galaxy. The correlations between the relative abundances of chemical elements and their second ionization potentials were calculated for groups of stars with effective temperatures between 3,764 and 7,725 K. Correlations were identified for chemical elements with second ionization potentials of 12.5 eV to 20 eV and for elements with second ionization potentials higher than 20 eV. For the first group of elements, the correlation coefficients were positive for stars with effective temperatures lower than 5,300 K and negative for stars with effective temperatures from 5,300 K to 7,725 K. The results of this study and the comparison with earlier results for hotter stars confirm the variations in these correlations with the effective temperature. A possible explanation for the observed effects is the accretion of hydrogen and helium atoms from the interstellar medium.
利用已发表的银河系本区域1149颗G和K巨星的恒星丰度图,研究了恒星大气中化学元素丰度相对于太阳丰度对相同元素二次电离势的依赖关系。计算了有效温度在3764 ~ 7725 K之间的恒星群中化学元素相对丰度与其第二电离势之间的相关性。第二电离势为12.5 eV至20 eV的化学元素和第二电离势高于20 eV的化学元素之间存在相关性。对于第一组元素,有效温度低于5300 K的恒星的相关系数为正,有效温度在5300 ~ 7725 K之间的恒星的相关系数为负。这项研究的结果以及与较热恒星的早期结果的比较证实了这些相关性与有效温度的变化。对于观测到的效应,一个可能的解释是来自星际介质的氢和氦原子的吸积。
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引用次数: 0
Magnetometer Calibration Based on the CHAOS-7 Model 基于混沌-7模型的磁强计标定
IF 0.5 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2021-08-15 DOI: 10.5140/JASS.2021.38.3.157
Hosub Song, Jaeheung Park, Jaejin Lee
We describe a method for the in-orbit calibration of body-mounted magnetometers based on the CHAOS-7 geomagnetic field model. The code is designed to find the true calibration parameters autonomously by using only the onboard magnetometer data and the corresponding CHAOS outputs. As the model output and satellite data have different coordinate systems, they are first transformed to a Star Tracker Coordinate (STC). Then, non-linear optimization processes are run to minimize the differences between the CHAOS-7 model and satellite data in the STC. The process finally searches out a suite of calibration parameters that can maximize the model-data agreement. These parameters include the instrument gain, offset, axis orthogonality, and Euler rotation matrices between the magnetometer frame and the STC. To validate the performance of the Python code, we first produce pseudo satellite data by convoluting CHAOS-7 model outputs with a prescribed set of the ‘true’ calibration parameters. Then, we let the code autonomously undistort the pseudo satellite data through optimization processes, which ultimately track down the initially prescribed calibration parameters. The reconstructed parameters are in good agreement with the prescribed (true) ones, which demonstrates that the code can be used for actual instrument data calibration. This study is performed using Python 3.8.5, NumPy 1.19.2, SciPy 1.6, AstroPy 4.2, SpacePy 0.2.1, and ChaosmagPy 0.5 including the CHAOS-7.6 geomagnetic field model. This code will be utilized for processing NextSat-1 and Small scale magNetospheric and Ionospheric Plasma Experiment (SNIPE) data in the future.
提出了一种基于CHAOS-7地磁场模型的体载磁强计在轨定标方法。该代码旨在通过仅使用板载磁强计数据和相应的CHAOS输出自动找到真正的校准参数。由于模型输出和卫星数据具有不同的坐标系,因此首先将它们转换为星跟踪器坐标(STC)。然后,运行非线性优化过程以最小化混沌7模型与STC中卫星数据之间的差异。该过程最终搜索出一套能最大限度地提高模型-数据一致性的校准参数。这些参数包括仪器增益、偏置、轴正交性和磁力计框架与STC之间的欧拉旋转矩阵。为了验证Python代码的性能,我们首先通过将CHAOS-7模型输出与一组规定的“真实”校准参数进行卷积来生成伪卫星数据。然后,我们让代码通过优化过程自动消除伪卫星数据的扭曲,最终跟踪到初始规定的校准参数。重建的参数与规定的(真实的)参数吻合较好,表明该代码可用于实际仪器数据的标定。本研究使用Python 3.8.5、NumPy 1.19.2、SciPy 1.6、AstroPy 4.2、SpacePy 0.2.1和ChaosmagPy 0.5进行,包括CHAOS-7.6地磁场模型。该代码将在未来用于处理NextSat-1和小尺度磁层和电离层等离子体实验(SNIPE)数据。
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引用次数: 2
The First Report on the Afternoon E -Region Plasma Density Irregularities in Middle Latitude 中纬度地区下午E区等离子体密度不规则性的首次报告
IF 0.5 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2021-06-01 DOI: 10.5140/JASS.2021.38.2.135
Tae-Yong Yang, Y. Kwak, Jaewook Lee, Jaeheung Park, Seonghwan Choi
We report, for the first time, the afternoon (i.e., from noon to sunset time) observations of the northern mid-latitude E-region field-aligned irregularities (FAIs) made by the very high frequency (VHF) coherent backscatter radar operated continuously since 29 December 2009 at Daejeon (36.18°N, 127.14°E, 26.7°N dip latitude) in South Korea. We present the statistical characteristics of the mid-latitude afternoon E-region FAIs based on the continuous radar observations. Echo signal-to-noise ratio (SNR) of the afternoon E-region FAIs is found to be as high as 35 dB, mostly occurring around 100–135 km altitudes. Most spectral widths of the afternoon echoes are close to zero, indicating that the irregularities during the afternoon time are not related to turbulent plasma motions. The occurrence of afternoon E-regional FAI is observed with significant seasonal variation, with a maximum in summer and a minimum in winter. Furthermore, to investigate the afternoon E-region FAIs- Sporadic E (Es) relationship, the FAIs have also been compared with Es parameters based on observations made from an ionosonde located at Icheon (37.14°N, 127.54°E, 27.7°N dip latitude), which is 100 km north of Daejeon. The virtual height of Es (h’Es) is mainly in the height range of 105 km to 110 km, which is 5 km to 10 km greater than the bottom of the FAI. There is no relationship between the FAI SNR and the highest frequencies (ftEs) (or blanket frequencies (fbEs)). SNR of FAIs, however, is found to be related well with (ftEs–fbEs).
本文首次报道了2009年12月29日以来,在韩国大田(36.18°N, 127.14°E, 26.7°N倾角)连续工作的甚高频(VHF)相干后向散射雷达对中纬度北部E区场向不规则(FAIs)的观测结果。基于连续雷达观测资料,给出了中纬度e区下午FAIs的统计特征。发现e区下午fai的回波信噪比(SNR)高达35 dB,主要发生在100-135 km高度附近。下午回波的频谱宽度大部分接近于零,表明下午时间的不规则性与湍流等离子体运动无关。下午e区域FAI的发生具有显著的季节变化,夏季最大,冬季最小。此外,为了研究下午E区fai -散发E (Es)的关系,fai还与Es参数进行了比较,这是基于位于大田以北100 km的利川(37.14°N, 127.54°E, 27.7°N)的电离层探空仪的观测结果。Es的虚拟高度主要在105 ~ 110 km之间,比FAI底部高5 ~ 10 km。FAI信噪比与最高频率(fte)(或覆盖频率(fbEs))之间没有关系。然而,发现fai的信噪比与(fte - fbes)密切相关。
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引用次数: 2
Resonance Capture for a Mercurian Orbiter in the Vicinity of Sun 在太阳附近的水星轨道器的共振捕获
IF 0.5 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2021-06-01 DOI: 10.5140/JASS.2021.38.2.93
E. H. Khattab, F. A. Abd El-Salam, W. A. Rahoma
In this work, the problem of resonance caused by some gravitational potentials due to Mercury and a third body, namely the Sun, together with some non-gravitational perturbations, specifically coronal mass ejections and solar wind in addition to radiation pressure, are investigated. Some simplifying assumptions without loss of accuracy are employed. The considered force model is constructed. Then the Delaunay canonical set is introduced. The Hamiltonian of the problem is obtained then it is expressed in terms of the Deluanay canonical set. The Hamiltonian is re-ordered to adopt it to the perturbation technique used to solve the problem. The Lie transform method is surveyed. The Hamiltonian is doubly averaged. The resonance capture is investigated. Finally, some numerical simulations are illustrated and are analyzed. Many resonant inclinations are revealed.
在这项工作中,研究了水星和第三个天体即太阳的一些引力势引起的共振问题,以及一些非引力扰动,特别是日冕物质抛射和太阳风以及辐射压力。采用了一些简化的假设,但不失准确性。构造了所考虑的力模型。然后引入了Delaunay正则集。得到了问题的哈密顿量,并用德鲁拉纳正则集表示。对哈密顿量进行重新排序,使其适用于用于解决问题的摄动技术。对李变换方法进行了研究。哈密顿是双重平均的。研究了共振捕获。最后,对一些数值模拟进行了说明和分析。许多共鸣的倾向显露出来。
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引用次数: 0
Ionization of Hydrogen in the Solar Atmosphere 太阳大气中氢的电离
IF 0.5 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2021-06-01 DOI: 10.5140/JASS.2021.38.2.83
J. Chae
The ionization degree of hydrogen is crucial in the physics of the plasma in the solar chromosphere. It specifically limits the range of plasma temperatures that can be determined from the Hα line. Given that the chromosphere greatly deviates from the local thermodynamic equilibrium (LTE) condition, precise determinations of hydrogen ionization require the solving of the full set of non-LTE radiative transfer equations throughout the atmosphere, which is usually a formidable task. In many cases, it is still necessary to obtain a quick estimate of hydrogen ionization without having to solve for the non-LTE radiative transfer. Here, we present a simple method to meet this need. We adopt the assumption that the photoionizing radiation field changes little over time, even if physical conditions change locally. With this assumption, the photoionization rate can be obtained from a published atmosphere model and can be used to determine the degree of hydrogen ionization when the temperature and electron density are specified. The application of our method indicates that in the chromospheric environment, plasma features contain more than 10% neutral hydrogen at temperatures lower than 17,000 K but less than 1% neutral hydrogen at temperatures higher than 23,000 K, implying that the hydrogen temperature determined from the Hα line is physically plausible if it is lower than 20,000 K, but may not be real, if it is higher than 25,000 K. We conclude that our method can be readily exploited to obtain a quick estimate of hydrogen ionization in plasma features in the solar chromosphere.
氢的电离度在太阳色球层等离子体的物理学中是至关重要的。它特别限制了等离子体温度的范围,可以从Hα线确定。考虑到色球极大地偏离了局部热力学平衡(LTE)条件,氢电离的精确测定需要求解整个大气的一整套非LTE辐射传输方程,这通常是一项艰巨的任务。在许多情况下,仍然有必要获得氢电离的快速估计,而不必求解非lte辐射传输。在这里,我们提出一种简单的方法来满足这一需求。我们假设,即使局部物理条件发生变化,光电离辐射场也不会随时间变化。有了这个假设,光电离率可以从一个已发表的大气模型中得到,当温度和电子密度给定时,光电离率可以用来确定氢的电离程度。我们的方法的应用表明,在色球环境中,在低于17000 K的温度下,等离子体特征含有10%以上的中性氢,而在高于23000 K的温度下,则含有不到1%的中性氢,这意味着从Hα线测定的氢温度在低于20000 K时在物理上是合理的,但如果高于25000 K,则可能不真实。我们的结论是,我们的方法可以很容易地利用,以获得在太阳色球中等离子体特征氢电离的快速估计。
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引用次数: 1
Preliminary Analysis on Launch Opportunities for Sun-Earth Lagrange Points Mission from NARO Space Center NARO航天中心日地拉格朗日点任务发射时机初步分析
IF 0.5 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2021-06-01 DOI: 10.5140/JASS.2021.38.2.145
Young-Joo Song, Donghun Lee
In this work, preliminary launch opportunities from NARO Space Center to the Sun-Earth Lagrange point are analyzed. Among five different Sun-Earth Lagrange points, L1 and L2 points are selected as suitable candidates for, respectively, solar and astrophysics missions. With high fidelity dynamics models, the L1 and L2 point targeting problem is formulated regarding the location of NARO Space Center and relevant Target Interface Point (TIP) for each different launch date is derived including launch injection energy per unit mass (C3), Right ascension of the injection orbit Apoapsis Vector (RAV) and Declination of the injection orbit Apoapsis Vector (DAV). Potential launch periods to achieve L1 and L2 transfer trajectory are also investigated regarding coasting characteristics from NARO Space Center. The magnitude of the Lagrange Orbit Insertion (LOI) burn, as well as the Orbit Maintenance (OM) maneuver to maintain more than one year of mission orbit around the Lagrange points, is also derived as an example. Even the current work has been made under many assumptions as there are no specific mission goals currently defined yet, so results from the current work could be a good starting point to extend diversities of future Korean deep-space missions.
分析了从NARO航天中心到日地拉格朗日点的初步发射时机。在5个不同的太阳-地球拉格朗日点中,选择L1点和L2点分别作为太阳和天体物理任务的合适候选者。利用高保真动力学模型,建立了NARO空间中心位置L1点和L2点定位问题,并推导了不同发射日期下的目标界面点(TIP),包括单位质量发射注入能量(C3)、注入轨道Apoapsis矢量(RAV)赤经和DAV赤纬。根据NARO航天中心的滑行特性,还研究了实现L1和L2转移轨迹的潜在发射周期。拉格朗日轨道插入(LOI)燃烧的量级,以及维持围绕拉格朗日点超过一年的任务轨道的轨道维护(OM)机动,也作为一个例子推导出来。即使是目前的工作,也没有确定具体的任务目标,因此,目前的工作成果可以成为扩大韩国未来深空任务多样性的良好起点。
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引用次数: 0
A Preliminary Impulsive Trajectory Design for (99942) Apophis Rendezvous Mission (99942)阿波菲斯交会任务脉冲轨迹初步设计
IF 0.5 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2021-06-01 DOI: 10.5140/JASS.2021.38.2.105
Pureum Kim, S. Park, Sungki Cho, J. Jo
In this study, a preliminary trajectory design is conducted for a conceptual spacecraft mission to a near-Earth asteroid (NEA) (99942) Apophis, which is expected to pass by Earth merely 32,000 km from the Earth’s surface in 2029. This close approach event will provide us with a unique opportunity to study changes induced in asteroids during close approaches to massive bodies, as well as the general properties of NEAs. The conceptual mission is set to arrive at and rendezvous with Apophis in 2028 for an advanced study of the asteroid, and some near-optimal (in terms of fuel consumption) trajectories under this mission architecture are to be investigated using a global optimization algorithm called monotonic basin hopping. It is shown that trajectories with a single swing-by from Venus or Earth, or even simpler ones without gravity assist, are the most feasible. In addition, launch opportunities in 2029 yield another possible strategy of leaving Earth around the 2029 close approach event and simply following the asteroid thereafter, which may be an alternative fuel-efficient option that can be adopted if advanced studies of Apophis are not required.
在这项研究中,对一颗近地小行星(NEA)(99942)阿波菲斯的概念性航天器任务进行了初步的轨道设计,该小行星预计将于2029年在距离地球表面仅32,000公里的地方经过地球。这次近距离接近事件将为我们提供一个独特的机会来研究小行星在近距离接近大质量天体时引起的变化,以及近地天体的一般特性。这一概念任务将于2028年抵达并与阿波菲斯会合,对这颗小行星进行深入研究。在这一任务架构下,一些接近最优(就燃料消耗而言)的轨迹将使用一种称为单调盆地跳跃的全局优化算法进行研究。研究表明,从金星或地球单次掠过的轨迹,甚至是没有重力辅助的更简单的轨迹,都是最可行的。此外,2029年的发射机会产生了另一种可能的策略,即在2029年接近事件前后离开地球,然后简单地跟随小行星,这可能是一种替代的节油选择,如果不需要对阿波菲斯进行高级研究,可以采用。
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引用次数: 2
Recovery of Asteroids from Observations of Too-Short Arcs by Triangulating Their Admissible Regions 用三角测量法从过短弧观测中恢复小行星的可容许区域
IF 0.5 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2021-06-01 DOI: 10.5140/JASS.2021.38.2.119
Daniela Espitia, E. Quintero, M. A. Parra
The data set collected during the night of the discovery of a minor body constitutes a too-short arc (TSA), resulting in failure of the differential correction procedure. This makes it necessary to recover the object during subsequent nights to gather more observations that will allow a preliminary orbit to be calculated. In this work, we present a recovery technique based on sampling the admissible region (AdRe) by the constrained Delaunay triangulation. We construct the AdRe in its topocentric and geocentric variants, using logarithmic and exponential metrics, for the following near-Earth-asteroids: (3122) Florence, (3200) Phaethon, 2003 GW, (1864) Daedalus, 2003 BH84 and 1977 QQ5; and the main-belt asteroids: (1738) Oosterhoff, (4690) Strasbourg, (555) Norma, 2006 SO375, 2003 GE55 and (32811) Apisaon. Using our sampling technique, we established the ephemeris region for these objects, using intervals of observation from 25 minutes up to 2 hours, with propagation times from 1 up to 47 days. All these objects were recoverable in a field of vision of 95’ × 72’, except for (3122) Florence and (3200) Phaethon, since they were observed during their closest approach to the Earth. In the case of 2006 SO375, we performed an additional test with only two observations separated by 2 minutes, achieving a recovery of up to 28 days after its discovery, which demonstrates the potential of our technique.
发现小天体当晚收集的数据集构成过短弧线(TSA),导致差分校正程序失败。这使得有必要在随后的夜晚恢复该物体,以收集更多的观测数据,从而计算出初步的轨道。在这项工作中,我们提出了一种基于约束Delaunay三角剖分采样允许区域(AdRe)的恢复技术。我们使用对数和指数度量,对以下近地小行星(3122)Florence, (3200) Phaethon, 2003 GW,(1864)代达罗斯,2003 BH84和1977 QQ5)构建了地心和地心变量的AdRe;和主带小行星:(1738)Oosterhoff, (4690) Strasbourg, (555) Norma, 2006 SO375, 2003 GE55和(32811)Apisaon。利用采样技术,我们建立了这些天体的星历区,观测间隔从25分钟到2小时不等,传播时间从1天到47天不等。除了(3122)佛罗伦萨和(3200)法厄同外,所有这些物体都是在95 ' × 72 '的视野范围内可恢复的,因为它们是在最接近地球的时候观察到的。在2006 SO375的案例中,我们进行了一次额外的测试,只进行了两次相隔2分钟的观察,在发现后的28天内实现了恢复,这证明了我们技术的潜力。
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引用次数: 0
Active Days around Solar Minimum and Solar Cycle Parameter 太阳极小期活动日与太阳周期参数
IF 0.5 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2021-03-01 DOI: 10.5140/JASS.2021.38.1.23
Heon-Young Chang
Utilizing a new version of the sunspot number and group sunspot number dataset available since 2015, we have statistically studied the relationship between solar activity parameters describing solar cycles and the slope of the linear relationship between the monthly sunspot numbers and the monthly number of active days in percentage (AD). As an effort of evaluating possibilities in use of the number of active days to predict solar activity, it is worthwhile to revisit and extend the analysis performed earlier. In calculating the Pearson’s linear correlation coefficient r, the Spearman’s rank-order correlation coefficient rs, and the Kendall’s τ coefficient with the rejection probability, we have calculated the slope for a given solar cycle in three different ways, namely, by counting the spotless day that occurred during the ascending phase and the descending phase of the solar cycle separately, and during the period corresponding to solar minimum ± 2 years as well. We have found that the maximum solar sunspot number of a given solar cycle and the duration of the ascending phase are hardly correlated with the slope of a linear function of the monthly sunspot numbers and AD. On the other hand, the duration of a solar cycle is found to be marginally correlated with the slope with the rejection probabilities less than a couple of percent. We have also attempted to compare the relation of the monthly sunspot numbers with AD for the even and odd solar cycles. It is inconclusive, however, that the slopes of the linear relationship between the monthly group numbers and AD are subject to the even and odd solar cycles.
利用2015年以来新版本的太阳黑子数和群黑子数数据集,我们统计研究了描述太阳周期的太阳活动参数与月黑子数与月活跃日数百分比(AD)之间线性关系的斜率之间的关系。为了评估利用活动日数来预测太阳活动的可能性,值得重新审视和扩展先前进行的分析。在计算皮尔逊线性相关系数r、斯皮尔曼秩序相关系数rs和肯德尔τ系数与拒绝概率时,我们用三种不同的方法计算了给定太阳周期的斜率,即分别计算太阳周期上升阶段和下降阶段以及太阳极小期±2年对应的时间段内的无黑天。我们发现,给定太阳周期的最大太阳黑子数和上升阶段的持续时间与月黑子数和AD的线性函数斜率几乎不相关。另一方面,太阳活动周期的持续时间被发现与坡度有些微相关,拒绝概率小于百分之几。我们也试着比较了在偶数和奇数太阳周期中,月黑子数与AD的关系。然而,月群数与AD之间线性关系的斜率是否受偶数和奇数太阳周期的影响尚不确定。
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引用次数: 0
Methodology for the Observations of Stellar Occultations by Small Bodies of the Solar System 太阳系小天体掩星观测方法
IF 0.5 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2021-03-01 DOI: 10.5140/JASS.2021.38.1.1
Luis E. Salazar-Manzano, E. Quintero
The observation of stellar occultations constitutes one of the most important techniques for determining the dimensions and establishing the physical parameters of small Solar System bodies. The most substantial calculations are obtained from multiple observations of the same event, which turns the observation of stellar occultations into highly collaborative work and groups teams of observers through international networks. The above situation also requires the participation of both professional and amateur observers in these collaborative networks. With the aim of promoting the participation of professional and amateur groups in the collaborative observation of stellar occultations, we present the methodology developed by the Astronomical Observatory of the Technological University of Pereira (OAUTP) for the observations of occultations due small Solar System bodies. We expose the three fundamental phases of the process: the plan to make observations, the capture of the events, and the treatment of the data. We apply our methodology using a fixed station and a mobile station to observe stellar occultations due to MBAs (354) Eleonora (61) Danae (15112) Arlenewolfe (3915) Fukushima (61788) 2000 QP181 (425) Cornelia (257) Silesia (386) Siegena and (41) Daphne, and due to TNOs 1998BU48 and (529823) 2010 PP81. The positive detections for the objects (257) Silesia (386) Siegena and (41) Daphne allow us to derive lower limits in the diameter of the MBAs of 63.1 km, 166.2 km and 158.7 km and offsets in the astrometric position (Δαc cosδc, Δδc) of 622.30 ± 0.83, 15.23 ± 9.88 mas, 586.06 ± 1.68, 43.03 ± 13.88 mas and –413.44 ± 9.42, 234.05 ± 19.12 mas, respectively.
对掩星的观测是确定太阳系小天体的尺寸和建立其物理参数的最重要的技术之一。最重要的计算是从对同一事件的多次观测中获得的,这使得对恒星掩星的观测成为高度协作的工作,并通过国际网络将观察者团队分组。上述情况还需要专业和业余观察者参与这些协作网络。为了促进专业和业余团体共同参与对恒星掩星的观测,我们提出了由佩雷拉科技大学天文台(OAUTP)开发的用于观测太阳系小天体掩星的方法。我们公开了该过程的三个基本阶段:进行观察的计划、捕获事件和处理数据。我们应用我们的方法,使用一个固定站和一个移动站来观测由于mba (354) Eleonora (61) Danae (15112) Arlenewolfe (3915) Fukushima (61788) 2000 QP181 (425) Cornelia (257) Silesia (386) Siegena和(41)Daphne以及由于TNOs 1998BU48和(529823)2010 PP81造成的掩星。通过对(257)Silesia (386) Siegena和(41)Daphne天体的阳性检测,我们得出了MBAs直径的下限分别为63.1 km、166.2 km和158.7 km,在天文测量位置(Δαc co - δc, Δδc)的偏移量分别为622.30±0.83、15.23±9.88 mas、586.06±1.68、43.03±13.88 mas和-413.44±9.42、234.05±19.12 mas。
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引用次数: 0
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