Origin of coronal and interplanetary shock and particle acceleration of a flare/CME event

By using radio data from ground-based telescopes (from 270 MHz to 25 MHz), and from the Radio and Plasma Wave experiment (WAVES) on board the WIND spacecraft (1–14 MHz and several kHz-11 MHz), as well as FY -2 satellite data, the origin of coronal and interplanetary shock and particle acceleration of the 14 July 2000 flare/CME event (the Bastille day event) have been studied. Main conclusions are as follows: (1) We investigate the causal relationship between metric type 11 bursts observed by the digital IZMIRAN radio spectrograph and type II radio emissions in the frequency range from 1–14 MHz and several kHz-11 MHz observed by the WAVES/WIND. The analysis indicate that the fast CME is the origin of both coronal and interplanetary shocks. (2)According to the time profiles of Hard X-ray, and energetic particles (include proton, ³He, and ⁴He) from FY-2 satellite, it is obvious that the Bastille day event is the event, in which both impulsive and gradual phenomena occur. The energetic particles accelerated not only in flare but also in CME.     

VHF radio response of the near Earth space during solar activity growth in October, 2003

The analysis of observations of very high frequency radio noise intensity at the middle latitude on a frequency f = 500 MHz from 14th till 26th of October, 2003 is presented. These data are compared with the solar radio bursts in the range of frequencies 1–14 MHz registered by RAD2 receiver of the WAVES device installed on board the WIND spacecraft.     

“嫦娥4号”任务有效载荷系统设计与实现

"嫦娥4号"任务将首次实现人类在月球背面软着陆。通过分析任务特点,以多类型有效载荷配置为背景,介绍了以科学目标和探测任务为核心的有效载荷系统设计思路和实现方法。同时针对首次在深空探测领域搭载国际合作有效载荷项目情况进行了说明。"嫦娥4号"任务最重要的科学目标是利用月球背面洁净的电磁环境进行天文低频射电观测,因此分别在着陆器和中继星上新增配置了国内新研制的低频射电频谱仪及荷兰研制的低频探测仪。科学探测的太阳爆发产生的低频电场信号极其微弱,如何消除着陆器和中继星上其他电子设备发射的近场噪声对远场探测信号的干扰就成了本次任务的最大难点。在相关研制单位的多方努力下,通过优化接收天线设计和地面数据处理算法等多种手段,实现了低频探测信号不低于30 d B的噪声抑制性能,具备了实现科学目标的能力。     

Solar origin of near-relativistic impulsiveelectron events

There is increasing evidence suggesting that coronal acceleration supplies at least part of the particles observed during solar energetic particle events, yet coronal processes tend to be mostly disregarded in these studies. This is often due to the fact that the coronal restructuring in the early development of the associated flare and/or coronal mass ejection event is extremely fast (on the order of a few minutes) and can encompass most of the solar disk, thus requiring a full disk solar imager with very high time-cadence, and wide spectral coverage. An important subset of the energetic particle events are the near-relativistic impulsive electron events detected near Earth: their onsets can be traced back to a release time in the low corona with accuracies on the order of a couple of minutes. We investigate a series of impulsive electron events from 1998 to 2001 using energetic electron data measured in situ by the Electron, Proton, and Alpha Monitor (EPAM) experiment on the Advanced Composition Explorer (ACE) spacecraft, and radio coronal observations from the Nanqay Radioheliograph, the Decametric Array from Nanqay and the WAVES experiment on the WIND spacecraft. EPAM measures electrons in the energy range from 40 to 300 keV over a wide range of look directions and with better than 1 minute time resolution, while the Nançay radioheliograph provides images of the solar corona at 5 different frequencies with time cadence of 8 images per second and per frequency. This study focuses on the events which correspond to a delay, between the inferred injection times of the electrons at the Sun, and the electromagnetic emissions from flares, of at least 5 minutes. Radio signatures are found near the estimated time of the electron release for each of the events. The timing and spectral characteristics of the radio emissions, when compared with the properties of the particles seen at EPAM, strongly support an acceleration process in the corona but at highly variable heights from one event to the other.     

一种针对金星探测器的姿态指向设计

摘要： 金星探测需要超长距离低码率传输,因而金星探测器需要保持其数传天线指向地球.相对于地球轨道飞行器来说,金星探测器距离太阳更近,需要固定散热面来维持探测器内的温度.提供一种基于在金星探测器偏置安装天线的姿态指向设计,能够保证从金星向地球传输数据并且维持散热面远离太阳.而此设计旨在减少数传天线的数量至一根同时将两个固定平面作为散热面.还提供两种详细方案来控制姿态机动来保证在数传天线始终指向地球的同时在特定节点切换散热面.     

Solar wind electron density and temperature over solar cycle 23: Thermal noise measurements on Wind

We present the solar wind plasma parameters obtained from the Wind spacecraft during more than nine years, encompassing almost the whole solar cycle 23. Since its launch in November 1994 Wind has frequently observed the in-ecliptic solar wind upstream of the Earth’s bow shock. The WIND/WAVES thermal noise receiver was specially designed to measure the in situ plasma thermal noise spectra, from which the electron density and temperature can be accurately determined. We present and discuss histograms of such measurements performed from 1994 to 2003. Using these large data sets, we study the density and core temperature variations with solar activity cycle and with different regimes of the solar wind. We confirm the anticorrelation of the electron density with the sunspot number, and obtain a positive correlation of the core temperature, with the sunspot number.     

WIND/3DP and Nancay radioheliographobservations of solar energetic electron events

Initial results of a combined study of electron events using the 3DP experiment on the WIND spacecraftand the Nançay Radioheliograph (NRH) are presented. A total of 57 electron events whose solar release time could be inferred from WIND/3DP observations occurred during NRH observing times. In 40 of them a distinct signature was detected in maps at decimetric and metric wavelengths (dm-m-λ) taken by the NRH. These events are equally distributed among two categories: (1) Electron release together with dm-m-λ bursts of a few minutes duration: these events are also accompanied by decametric-hectometric type III bursts seen by WAVES/WIND. They correspond to the well-known impulsive electron events. (2) Electron release during long duration (several tens of minutes) dm-m-λ emission: the electrons are most often released more than ten minutes after the start of the radio event. In the majority of cases the dm-m-λ radio source changes position, size, and/or intensity near the time of electron release.     

航天器天线技术的特点和进展

<正> 航天器天线亦称空间飞行器天线,用于卫星、飞船、空间站和深空探测器。天线按功能分类有遥测、指令、跟踪、测速、数据中继、通信广播、科学探测、遥感、测向、交会雷达、着陆导航等等,其型式多种多样,工作频率从甚低频到毫米波段。航天器天线有时比航天器本体大得多(例如ATS—6,TDRS),有时几乎就是航天器大部分表面(例如Transit-1)。     

稻城太阳射电望远镜（DSRT）天线遮挡效应仿真

稻城太阳射电望远镜（DSRT）由313面6 m直径抛物面天线组成。天线接收信号幅值和相位的精确修正是决定DSRT成像质量的关键因素。然而DSRT阵列可能会出现邻近天线相互遮挡的问题，从而改变接收信号的幅值和相位，影响其成像质量。利用电磁仿真软件计算了接收频率为300 MHz（波长λ=1 m）时的相邻两单元与相邻三单元两种情况。三元系统中遮挡效应的影响仅比双元系统中相关影响略为显著。在本文考虑的最严重的遮挡情况（天线边缘的投影间距D = –1λ）下，对于双/三元系统，相对于单天线系统水平和垂直增益分别降低了0.6/0.6 dB和 0.3/0.4 dB，相位偏差分别为–3.3o/–3.871o和–1.744o/–2.244o。此外还分析了其他遮挡情况。研究表明DSRT系统中的天线遮挡效应分析可由双元系统充分描述，在后期数据处理时应适当考虑该效应，尽量提升DSRT数据的利用效率和成图质量。      

航天器天线有关技术的论述

论述了航天器天线的特点及其与航天器总体的关系;天线的辐射场方向图及增益有关问题;天线的电磁兼容及天线的计算机辅助设计。     

Multi-scale reconnections in a complex CME

A series of three flares of GOES class M, M and C, and a CME were observed on 20 January 2004 occurring in close succession in NOAA 10540. Types II, III, and N radio bursts were associated. We use the combined observations from TRACE, EIT, Hα images from Kwasan Observatory, MDI magnetograms, GOES, and radio observations from Culgoora and Wind/ WAVES to understand the complex development of this event. We reach three main conclusions. First, we link the first two impulsive flares to tether-cutting reconnections and the launch of the CME. This complex observation shows that impulsive quadrupolar flares can be eruptive. Second, we relate the last of the flares, an LDE, to the relaxation phase following forced reconnections between the erupting flux rope and neighbouring magnetic field lines, when reconnection reverses and restores some of the pre-eruption magnetic connectivities. Finally, we show that reconnection with the magnetic structure of a previous CME launched about 8 h earlier injects electrons into open field lines having a local dip and apex (located at about six solar radii height). This is observed as an N-burst at decametre radio wavelengths. The dipped shape of these field lines is due to large-scale magnetic reconnection between expanding magnetic loops and open field lines of a neighbouring streamer. This particular situation explains why this is the first N-burst ever observed at long radio wavelengths.     

深空测控网干涉测量系统在“鹊桥”任务中的应用分析

在"嫦娥4号"任务的第一阶段—"鹊桥"阶段,北京航天飞行控制中心利用佳木斯及喀什深空站对"鹊桥"进行了干涉测量观测,获取了实时与事后的高精度测角观测量,有效支持了任务的实施。两深空站需同时完成测控任务,无法交替射电源观测来进行系统差标校,基于此系统采用了长时间隔、在航天器观测前及双站结束后观测射电源的标校方法,在地月转移段、月球至L2转移段、Halo轨道形成段开展了多次干涉测量观测,所获得的时延、时延率结果直接应用于事后联合轨道确定,结果表明:深空网的时延观测精度约为3 ns。     

Orbit Design for Twin-spacecraft Space VLBI

Space Very Long Baseline Interferometry (S-VLBI) is an aperture synthesis technique utilizing an array of radio telescopes including ground telescopes and space orbiting telescopes. It can achieve much higher spatial resolution than that from the ground-only VLBI. In this paper, a new concept of twin spacecraft S-VLBI has been proposed, which utilizes the space-space baselines formed by two satellites to obtain larger and uniform uv coverage without atmospheric influence and hence achieve high quality images with higher angular resolution. The orbit selections of the two satellites are investigated. The imaging performance and actual launch conditions are all taken into account in orbit designing of the twin spacecraft S-VLBI. Three schemes of orbit design using traditional elliptical orbits and circular orbits are presented. These design results can be used for different scientific goals. Furthermore, these designing ideas can provide useful references for the future Chinese millimeter-wave S-VLBI mission.      

Two-velocity structure observed in the inner solar wind

Measurements of the motion of plasma density inhomogeneities in the inner solar wind are presented. The speeds were estimated using a cross-correlation analysis of radio frequency fluctuations of the Galileo spacecraft measured simultaneously at widely spaced ground stations. The radial projections of the correlation baselines on the pattern plane were of the order of several thousand kilometers. For cross-correlation functions calculated with comparatively short averaging times, we find that a pronounced two-velocity configuration is occasionally observed over the range of heliocentric distances 20 R < R < 40 R. The typical mean speed for such observations is about 300–400 km/s and the difference between the two predominant speeds is about 150–200 km/s. These results may indicate that the density fluctuations are associated with slow magnetosonic waves propagating in opposite directions at the local speed of sound in the reference frame moving with the mean solar wind speed. Quite reasonable estimates of the solar wind speed and speed of sound are obtained from this model. Another possible explanation of the two-velocity structures is that two independent solar wind streams are present simultaneously along different segments of the radio ray path.     

2006年12月13日太阳射电暴对GPS观测的影响

日地空间环境不仅影响航天器运行和安全, 也是导航、定位和通信等无线 电应用系统主要的误差源. 其中来自太阳L波段的射电暴被认为是全球导航卫星 系统(GNSS)稳定和性能的潜在威胁因素, 当L波段射电爆发达到一定阈值时, 将给用户带来不同程度的射电噪声干扰, 严重时会引起接收机失锁和定位服务 中断. 本文对2006年12月13日太阳射电暴对GPS造成的影响进行了研究, 利用太阳射电 观测数据、L波段闪烁观测数据和向阳面不同区域的GPS观测网数据, 分析 GPS观测对射电暴的响应. 结果表明, 此次事件对GPS观测产生了明显的影响, 射 电暴期间GPS发生幅度闪烁事件和明显失锁现象, 多个台站上空的多颗GPS 卫星 信号完全中断长达6min左右, 且多个台站上空锁定的卫星数目小于4颗, 使 得GPS定位完全失效. 相对而言, 射电暴期间日下点附近的GPS台站受到的影响 比远离日下点的大.      

深空探测器大口径天线指向在轨标定方案

基于深空探测器配备的大口径天线的指向精度要求,给出了一种深空探测器大口径天线在轨指向的标定方案,以解决深空探测器安装的大口径天线的在轨指向评价问题。通过对飞行器特点和约束条件的分析,结合"嫦娥4号"中继星天线的具体情况,采用星地协同工作的方法,给出了天线指向在轨标定的方案,并明确了标定的实施流程,最后对标定过程中的误差情况进行了分析。本方案可推广应用于其他深空探测器大口径天线指向标定方案的设计。     

Analysis of NASA’s DSN Venus Express radio occultation data for year 2014

The Venus Express Radio Science Experiment (VeRa) was part of the scientific payload of the Venus Express (VEX) spacecraft and was targeted at the investigation of Venus’ atmosphere, surface, and gravity field as well as the interplanetary medium. This paper describes the methods and the required calibrations applied to VEX-VeRa raw radio occultation data used to retrieve vertical profiles of Venus’ ionosphere and neutral atmosphere. In this work we perform an independent analysis of a set of 25 VEX, single-frequency (X-band), occultations carried out in 2014, recorded in open-loop at the NASA Deep Space Network. Our temperature, pressure and electron density vertical profiles are in agreement with previous studies available in the literature. Furthermore, our analysis shows that Venus’ ionosphere is more influenced by the day/night condition than the latitude variations, while the neutral atmosphere experiences the opposite. Our scientific interpretation of these results is based on two major responsible effects: Venus’ high thermal inertia and the zonal winds. Their presence within Venus’ neutral atmosphere determine why in these regions a latitude dependence is predominant on the day/night condition. On the contrary, at higher altitudes the two aforementioned effects are less important or null, and Venus’ ionosphere shows higher electron density peaks in the probed day-time occultations, regardless of the latitude.     

两飞行器间无线数据链通信区域建模

为实现两飞行器在飞行过程中的正常通信,需建立一套通信区域的计算模型.基于空地无线数据链通信,从其实现正常通信的条件出发,考虑通信链路中的发射机、接收机、收发天线、传输空间及地球曲率、飞行器姿态角以及飞行器的空间位置关系等因素,分析研究了飞行器间无线数据链通信区域,建立了两飞行器间无线数据链通信区域的数学模型,包括天线、飞行高度、两飞行器空间位置关系、通信区域模型等.该模型已成功应用于某型号,为分析建立在无线数据链通信方式基础上的空地无线传输系统通信区域提供了参考,也适用于飞船、卫星等其它空空、空地无线数据通信系统.     

十字交叉振子类型圆极化天线的研究

通过对Ｈａｌｌｅｎ方程进行矩量法求解，讨论了十字交叉振子类型天线产生圆极化辐射时两对振子长度选择的方法；计算了几种情况下天线的远区辐射场；指出十字交叉振子、伞型振子等这类天线由于具有结构紧凑、工作可靠、易于赋形等特点，可广泛应用在空间飞行器上。     

A multi-wavelength study of the merger candidate Abell S0721 and the activities of its member galaxies

We present a multi-wavelength study of the merging history and its influence on galaxy activities of a newly detected merger candidate – Abell S0721. This cluster was only known as a poor cluster in the Shapley Supercluster, but when several survey data of different wavelengths are combined, evidence of strong merging is revealed. We have analyzed the optical and X-ray structures of the cluster, as well as galaxy dynamics and properties of the radio galaxies in the cluster. The dynamics analysis shows the velocity distribution of this system is significantly deviated from a 1-Gaussian model, indicating the existence of 2–3 dynamically different sub-systems; in addition, both optical and X-ray structures of the cluster show an elongated and multi-clump structure, two X-ray clumps imaged by ROSAT All Sky Survey are well correlated with two galaxy density peaks. This cluster is possibly a merger of several groups; our analysis shows that the projection angle for two clumps in the main structure is possibly near the projection plane, and the substructure is seen at ∼30–75° from the projection plane. The merging process could also be the origin to boost the activities of its member galaxies. Finally, as compared with other merger candidates in the Shapley Supercluster, the radio galaxies identified in Abell S0721 are all optically luminous, and the fraction of luminous radio galaxies is only lower than one merger candidate (which is proposed to be at the very beginning of a merger event), this suggests Abell S0721 is also at the beginning of a merger event.