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1.
ＮＥＡＲ将近探爱神星许梅美国宇航局于１９９６年２月１６日发射了一艘近地小行星探测飞船（Ｎｅａｒ－ＥａｒｔｈＡｓｔｅｒｏｉｄＲｅｎｄｅｚｖｏｕｓＳｐａｃｅｃｒａｆｔ,缩写为ＮＥＡＲ）,其主要探测目标为第４３３号近地小行星爱神星（Ｅｒｏｓ）,预定飞船将... 相似文献
2.
为满足大气模型比较的需要，把ＣＩＲＡ－１９８６大气模式（简称ＣＩＲＡ８６）引入大气阻力选择模块，对上海天文台人造卫星精密定轨软件ＳＨＯＲＤＥ进行大气模式的扩充。利用多种大气模式分别对Ｓｔａｒｌｅｔｔｅ卫星的观测资料进行解算，结果表明：ＳＨＯＲＤＥ中指数大气模式更适合对Ｓｔａｒｌｅｔｔｅ卫星进行精密定轨研究。 相似文献
3.
为满足大气模型比较的需要，把ＣＩＲＡ－１９８６大气模式（简称ＣＩＲＡ８６）引入大气阻力选择模块，对上海天文台人造卫星精密定轨软件ＳＨＯＲＤＥ［１］进行大气模式的扩充。利用多种大气模式分别对Ｓｔａｒｌｅｔｅ卫星的观测资料进行解算，结果表明：ＳＨＯＲＤＥ中指数大气模式更适合对Ｓｔａｒｌｅｔｅ卫星进行精密定轨研究 相似文献
4.
在对恒星形成区（ＳＦＲ）中ＲＯＳＡＴ选弱发射线ＴＴａｕｒｉ星（ＷＴＴＳ）进行光谱证认的过程中,发展了一套基于北京天文台２．１６米光学望远镜及其ＯＭＲ卡焦光谱仪系统的晚型星中色散（５０Ａ／ｍｍ）光谱计算机自动光谱分类方法．对ＲＯＳＡＴ选ＷＴＴＳ候选作中晚型星进行自动光谱分类的结果表明,一般情况下,光谱型的分类精度可达±１个次级,个别源为±２个次级．该自动光谱分类方法同时适用于其他光谱晚型星． 相似文献
5.
晚型星计算机自动光谱分类 总被引：1，自引：1，他引：0
在对恒星形成区（ＳＦＲ）中ＲＯＳＡＴ选弱发射线Ｔ Ｔａｕｒｉ星（ＷＴＴＳ）进行光谱证认的过程中,发展了一套基于北京天台２．１６米光学望远镜及其ＯＭＲ卡焦光谱仪系统的晚型星中色散（５０Ａ／ｍｍ）光谱计算机自动光谱分类方法。对ＲＯＳＡＴ选ＷＴＴＳ候选体中晚型星进行自动光谱分类的结果表明,一般情况下,光谱型的分类精度可达±１个次级,个别源为±２个次级。该自动光谱分类方法同时适用于其它光谱晚型星。 相似文献
6.
分析ＲＸＴＥ卫星ＰＣＡ探测器对ＣｙｇＸ－１的观测数据,得到了其处于高态及高低高转换时的Ｘ射线短时标爆发（Ｓｈｏｔ）结构。在所观测到的三种态中是不对称的,并且不同的状态中Ｓｈｏｔ的结构有明显差异。Ｓｈｏｔ前后沿可分别由双指数函数近似拟合。Ｓｈｏｔ中的快时变过程是由慢的上升前沿和快的下降后沿构成。在所观测态中Ｓｈｏｔ平均宽度约为０．１１秒（ＦＷＨＭ）,比低态时的宽度窄。同一状态中高能段的Ｓｈｏｔ宽度较 相似文献
7.
１９９８年９月２０日,伦琴Ｘ射线天文卫星（ＲＯＳＡＴ）在指向转换过程中扫过太阳附近,结果来自太阳的强烈Ｘ射线烧毁了其上的高分辨成像仪（ＨＲＩ）。此后,在１９９８年１２月,ＲＯＳＡＴ上的另一个主要探测器位置灵敏正比计数器（ＰＳＰＣ）利用剩余的少量气体进... 相似文献
8.
新发现的4个X选类星体和2个赛弗特星系 总被引：2，自引：1，他引：1
１９９７－１９９８年期间,使用２．１６ｍ望远镜对ＲＯＳＡＴ Ｘ射线源进行光学证认,证认出４个ＲＯＳＡＴ Ｘ射线源是新发现的类星体,２个ＲＯＳＡＴ Ｘ射线源是新发现的赛弗特星系。 相似文献
9.
本文利用Ｂｅｒｔｅｌｉ等人新算出的等龄线，以及Ｇｕｎｎ和Ｓｔｒｙｋｅｒ观测的恒星光谱（３１３０－１０８００）构造了一个星族综合模型．该模型能预计金属丰度在Ｚ＝０．０００４－０．０５，年龄在１０７－２×１０１０年范围内的简单星族（ＳＳＰ）的光谱能量分布（ＳＥＤ）．利用ＳＳＰ，通过对不同时刻恒星形成率的卷积能够得到星系的ＳＥＤ的演化．我们计算出ＳＳＰ以及星系在ＵＢＶＲＩ系统和ＢＡＴＣ１５色中带测光系统中的颜色．计算出的从Ｅ／ＳＯ到Ｓｄｍ各类星系的ＵＢＶＲＩ颜色在年龄为１２Ｇｙｒ时都和观测符合较好．因此，我们的模型为正在进行的关于星系ＳＥＤ的多色测光研究提供了理论上的探索． 相似文献
10.
11.
Zhang Fei-peng Huang Cheng Feng Chu-gang Dong Xiao-jun Liao Xin-hao 《Chinese Astronomy and Astrophysics》2001,25(4):641-489
Variance component estimation (VCE) is applied to precise orbit determination (POD) of the ERS-2 satellite. Twenty 5-day long arcs in the early three months in 1998 were calculated using the SLR and PRARE data. In the data the adjacent arcs overlap for two days except the intervals for orbit maneuver. The effect of VCE orbit determination on the calculation is investigated by an analysis of residuals and comparison of overlapping arcs, and the mean a posteriori standard deviation of each group of measured residuals is given. It is shown by the residuals analysis that the fitting of the measurements is significantly improved by VCD. However, according to Abbey criterion, VCD is not able to eliminate the systematic errors due to errors in the dynamic and geometric models. The results of the comparison of the overlapping arcs show that (1) VCE reduces the mean range deviation of overlapping arcs, especially where there are obviously unreasonable deviations, so that the orbit obtained has a more uniform precision; (2) By using VCE, adjacent arcs tend to close up and this is more apparent in the transverse direction. From the mean a posteriori standard error of each group of measurements, it can be seen that as far as the single normal point measurement is concerned, the data of some SLR stations are more important than other measurements in POD calculation. Generally speaking, determination of weighting by using VCE is more reasonable than by using initial standard deviation. 相似文献
12.
A. F. Dravskikh A. M. Finkelstein G. A. Krasinsky 《Astrophysics and Space Science》1975,38(2):255-266
The aim of this paper has been to discuss a possibility of the formation of an inertial system of coordinates, precise within 0″.001, with the aid of the measures of mutual angular distances of quasars by the VLBI technique used in radio-astronomy. Such a system depends on neither the rotation, nor revolution of the Earth around the Sun — a fact which permits a separation of the astronomical and geophysical aspects of the problem. The proposed system should permit us to resolve some general astrometric problems — such as of the precession and nutation of the Earth as well as of the motion of the terrestrial axis of rotation within the Earth, or fluctuations in the angular veoocity of terrestrial rotation. 相似文献
13.
Jana Ticha Milos Tichy Michal Kocer Michaela Honkova 《Meteoritics & planetary science》2009,44(12):1889-1895
Abstract— Near‐Earth object (NEO) research plays an increasingly important role not only in solar system science but also in protecting our planetary environment as well as human society from the asteroid and comet hazard. Consequently, interest in detecting, tracking, cataloguing, and the physical characterizing of these bodies has steadily grown. The discovery rate of current NEO surveys reflects progressive improvement in a number of technical areas. An integral part of NEO discovery is astrometric follow‐up crucial for precise orbit computation and for the reasonable judging of future close encounters with the Earth, including possible impact solutions. The KLENOT Project of the Klet Observatory (South Bohemia, Czech Republic) is aimed especially at the confirmation, early follow‐up, long‐arc follow‐up, and recovery of near‐Earth objects. It ranks among the world's most prolific professional NEO follow‐up programs. The 1.06 m KLENOT telescope, put into regular operation in 2002, is the largest telescope in Europe used exclusively for observations of minor planets and comets, and full observing time is dedicated to the KLENOT team. In this paper, we present the equipment, technology, software, observing strategy, and results of the KLENOT Project obtained during its first phase from March 2002 to September 2008. The results consist of thousands of precise astrometric measurements of NEOs and also three newly discovered near‐Earth asteroids. Finally, we also discuss future plans reflecting also the role of astrometric follow‐up in connection with the modus operandi of the next generation surveys. 相似文献
14.
R. M. Weisman M. Majji K. T. Alfriend 《Celestial Mechanics and Dynamical Astronomy》2014,118(2):165-195
This paper presents an approach to characterize the uncertainty associated with the state vector obtained from the Herrick-Gibbs orbit determination approach using transformation of variables. The approach is applied to estimate the state vector and its probability density function for objects in low Earth orbit using sparse observations. The state vector and associated uncertainty estimates are computed in Cartesian coordinates and Keplerian elements. The approach is then extended to accommodate the $J_2$ perturbation where the state vector is written in terms of mean orbital elements. The results obtained from the analytical approach presented in this paper are validated using Monte Carlo simulations and compared with the often utilized similarity transformation for Kepler, mean, and nonsingular elements. The measurement uncertainty characterization obtained is used to initialize conventional nonlinear filters as well as operate a Bayesian approach for orbit determination and object tracking. 相似文献
15.
M. D. Campbell-Brown S. Close 《Monthly notices of the Royal Astronomical Society》2007,382(3):1309-1316
The Advanced Research Project Agency (ARPA) Long Range Tracking and Instrumentation Radar has recorded thousands of head echoes from small meteoroids, which include detailed trajectory information as well as ionization measurements. In total, 25 complete ionization curves have been matched using a detailed model of meteoroid ablation, though the solutions are not necessarily unique. While measurements of the spread along the trajectory of the echoes indicate that most meteors in this size range do not have large separations among fragments, the ionization curves are consistent with fragmenting bodies in the most cases. Very precise radar measurements of meteors can be a valuable source of data on the chemical and physical properties of small meteoroids. 相似文献
16.
A New Ionosphere Monitoring Technology Based on GPS 总被引：1，自引：0，他引：1
Claudio Brunini Amalia Meza Francisco Azpilicueta María Andrea Van Zele Mauricio Gende Alejandro Díaz 《Astrophysics and Space Science》2004,290(3-4):415-429
Although global positioning system (GPS) was originally planned as a satellite-based radio-navigation system for military purposes, civilian users have significantly increased their access to the system for both, commercial and scientific applications. Almost 400 permanent GPS tracking stations have been stablished around the globe with the main purpose of supporting scientific research. In addition, several GPS receivers on board of low Earth orbit satellites fitted with special antennas that focus on Earth's horizon, are tracking the radio signals broadcasted by the high-orbiting GPS satellites, as they rise and set on Earth horizon. The data of these ground and space-born GPS receivers, readily accessible through Internet in a ‘virtual observatory’ managed by the International GPS Service, are extensively used for many researches and might possibly ignite a revolution in Earth remote sensing. By measuring the changes in the time it takes for the GPS signals to arrive at the receiver as they travel through Earth's atmosphere, scientists can derive a surprising amount of information about the Earth's ionosphere, a turbulent shroud of charged particles that, when stimulated by solar flares, can disrupt communications around the world. This contribution presents a methodology to obtain high temporal resolution images of the ionospheric electron content that lead to two-dimensional vertical total electron content maps and three-dimensional electron density distribution. Some exemplifying results are shown at the end of the paper. 相似文献
17.
James G. Williams 《Celestial Mechanics and Dynamical Astronomy》2018,130(10):63
The analysis of range or Doppler data between sites on the Earth and Moon requires an accurate computation of the lunar orbit and detailed models of the orientation of the Earth and Moon. Models constructed to understand range and range rate can lack detail, but if they include the largest lunar orbit variations, tracking stations on a rotating Earth, and lunar sites on a synchronously rotating Moon, then they will display the largest effects for orbit elements, Earth orientation, tracking station locations, and lunar site coordinates. The range and range rate are expanded into periodic series. To understand accurate solutions, the largest periodic terms that are sensitive to various solution parameters indicate the sensitivity of data to solution parameters and the time spans needed for their determination. Conclusions include: cylindrical coordinates work well for sites on the rapidly rotating Earth, but Cartesian coordinates are more natural for the synchronously rotating Moon since the series for the three coordinate projections are distinct. For range and range rate data, daily, semimonthly, monthly, and longer periods are present. For Doppler data, the daily periods may be stronger and more useful than the long periods, particularly for terms associated with the terrestrial tracking station. Doppler data do not determine the lander coordinate toward the Earth well. Observational strategies for range and Doppler data are not identical. For all data types, one wishes a variety of hour angles, lunar declinations, times of month, and longer periods. A long span of high-quality range data can improve the lunar orbit, orientation of the Earth’s equator, and physical librations. The locations of new lunar sites or new tracking stations can be determined from shorter spans of data. 相似文献
18.
《New Astronomy》2020
In March 2019 the first dedicated of optical observation of space debris and artificial satellites (Optical Satellites Tracking Station (OSTS)) in Egypt has been performed by National Research Institute of Astronomy and Geophysics (NRIAG) at Kottamia Observatory. The 0.28 m Telescope is used for tracking and surveying debris and operational satellites at Low Earth Orbit (LEO), High ellipse orbit (HEO) and the Geosynchronous Earth Orbit (GEO). OSTS has also collaborated with International Scientific Optical Network (ISON) for optical observation. The necessary programs to control the telescope, camera and monitoring process are configured. Coordinate corrected metric data is provided with the time information. The system has validated and calibrated processing. The first results of the observations with image processing using Apex-2 software are presented. The optical observations using OSTS are being used to help characterize the debris environment in LEO, HEO and GEO to assist in the modeling projections for space debris database, real population and distribution, detection and orbital determination, and conjunction analysis between operational satellites and/or dangers debris. 相似文献
19.
初步探讨用日长和卫星轨道摄动方法研究半月潮Mf 和月潮Mm 的Love数k2 .结果表明 ,日长方法给出k2 =0 .30 32 i0 .0 0 2 8(Mf) ,0 .30 2 6 i0 .0 0 1 2 (Mm) ,卫星轨道摄动方法为k2 =0 .30 83-i0 .0 1 0 0 (Mf) ,0 .30 1 4-i0 .0 0 1 0 (Mm) ,并与理论固体潮计算结果较为相符 .另外 ,上述结果更接近滞弹地球模型计算的结果 ,因此精确地测定长期潮Love数将对固体潮理论和地幔滞弹性提供重要的结束 . 相似文献
20.
Accurate Mars Express orbits to improve the determination of the mass and ephemeris of the Martian moons 总被引：1，自引：0，他引：1
P. Rosenblatt V. Lainey S. Le Maistre J.C. Marty V. Dehant M. Ptzold T. Van Hoolst B. Husler 《Planetary and Space Science》2008,56(7):1043-1053
The determination of the ephemeris of the Martian moons has benefited from observations of their plane-of-sky positions derived from images taken by cameras onboard spacecraft orbiting Mars. Images obtained by the Super Resolution Camera (SRC) onboard Mars Express (MEX) have been used to derive moon positions relative to Mars on the basis of a fit of a complete dynamical model of their motion around Mars. Since, these positions are computed from the relative position of the spacecraft when the images are taken, those positions need to be known as accurately as possible. An accurate MEX orbit is obtained by fitting two years of tracking data of the Mars Express Radio Science (MaRS) experiment onboard MEX. The average accuracy of the orbits has been estimated to be around 20–25 m. From these orbits, we have re-derived the positions of Phobos and Deimos at the epoch of the SRC observations and compared them with the positions derived by using the MEX orbits provided by the ESOC navigation team. After fit of the orbital model of Phobos and Deimos, the gain in precision in the Phobos position is roughly 30 m, corresponding to the estimated gain of accuracy of the MEX orbits. A new solution of the GM of the Martian moons has also been obtained from the accurate MEX orbits, which is consistent with previous solutions and, for Phobos, is more precise than the solution from the Mars Global Surveyor (MGS) and Mars Odyssey (ODY) tracking data. It will be further improved with data from MEX-Phobos closer encounters (at a distance less than 300 km). This study also demonstrates the advantage of combining observations of the moon positions from a spacecraft and from the Earth to assess the real accuracy of the spacecraft orbit. In turn, the natural satellite ephemerides can be improved and participate to a better knowledge of the origin and evolution of the Martian moons. 相似文献