IP over CCSDS/AOS空间通信QoS保证方法

首先分析空间通信体系发展趋势,提出基于IP over CCSDS/AOS的空间通信模型。在分析总结了地面网QoS(服务质量)机制和AOS(高级在轨系统)虚拟信道调度机制的基础上,提出一种IP(互联网协议)网络层区分服务与数据链路层AOS虚拟信道动态调度相结合的QoS保证方法。该方法将网络层的业务等级划分映射到AOS的虚拟信道分配算法中,并在此基础上实现AOS虚拟信道的动态调度,提高包括话音、视频在内的综合业务在空间链路传输的性能。     

Variability of the ionosphere over Irkutsk at low solar activity

Statistical and spectral analyses are performed to investigate variations of two ionosphere F2 layer key parameters, the critical frequency (foF2) and the peak height (hmF2), that were measured over Irkutsk (52.5°N, 104.0°E) from December 2006 to January 2008 under solar minimum. The analyses showed that both parameters contain quasi-harmonic oscillations with periods of T_n = 24/n hours (n = 1–7), among which the diurnal (n = 1) and semidiurnal (n = 2) ones are the strongest. Seasonal variations are explored of mean and median values, spectrum, amplitude, and phase of the diurnal and semidiurnal components of foF2 and hmF2.     

Disturbances in the ionospheric F-region peak heights in the American longitudinal sector during geomagnetic storms of September 2005

In this paper, we use the modified GSM TIP model to explore how the thermosphere–ionosphere system in the American longitudinal sector responded to the series of geomagnetic storms on September 9–14, 2005. Comparison of modeling results with experimental data at Millstone Hill, USA (42.6°N, 71.5°W), Ramey, Puerto Rico (18.3°N, 66.8°W) and Jicamarca, Peru (11.9°S, 76.9°W) has shown a good agreement of ionospheric disturbances in the F-region maximum height. We examine in detail the formation mechanisms of these disturbances at different latitudes and describe some of the important physical processes affecting the behavior of the F-region. In addition, we consider the propagation of thermospheric wind surge and the formation of additional layers in the low-latitude ionosphere during geomagnetic storms.     

A multiple-rendezvous,sample-return mission to two near-Earth asteroids

We propose a dual-rendezvous mission, targeting near-Earth asteroids, including sample-return. The mission, Asteroid Sampling Mission (ASM), consists of two parts: (i) flyby and remote sensing of a Q-type asteroid, and (ii) sampling of a V-type asteroid. The targeted undifferentiated Q-type are found mainly in the near-Earth space, and to this date have not been the target of a space mission. We have chosen, for our sampling target, an asteroid from the basaltic class (V-type), as asteroids in this class exhibit spectral signatures that resemble those of the well-studied Howardite–Eucrite–Diogenite (HED) meteorite suite. With this mission, we expect to answer specific questions about the links between differentiated meteorites and asteroids, as well as gain further insight into the broader issues of early Solar System (SS) evolution and the formation of terrestrial planets. To achieve the mission, we designed a spacecraft with a dry mass of less than 3 tonnes that uses electric propulsion with a solar-electric power supply of 15 kW at 1 Astronomical Unit (AU). The mission includes a series of remote sensing instruments, envisages landing of the whole spacecraft on the sampling target, and employs an innovative sampling mechanism. Launch is foreseen to occur in 2018, as the designed timetable, and the mission would last about 10 years, bringing back a 150 g subsurface sample within a small re-entry capsule. This paper is a work presented at the 2008 Summer School Alpbach,“Sample return from the Moon, asteroids and comets” organized by the Aeronautics and Space Agency of the Austrian Research Promotion Agency. It is co-sponsored by ESA and the national space authorities of its Member and Co-operating States, with the support of the International Space Science Institute and Austrospace.     

北斗导航系统在物联网中的应用展望

物联网是信息技术领域又一个重要发展,它使传统网络从人与人的联系扩展到物与物、物与人的联系。北斗导航系统是我国正在建设的全球卫星导航系统。分析北斗导航系统在物联网中应用的可行性,从物联网的组成结构出发,分析北斗导航系统相比于传统电信网络的优势,并对北斗导航系统在物联网中的应用模式进行展望。     

航空精密工件电火花加工微型方窗口研究

在电火花加工中,零件参数的选择对加工工艺指标起着重要作用,只有正确选择电参数才能加工出品质优良的产品。影响电参数选择的因素主要有:电极材料、工件材料、放电面积、表面粗糙度、放电间隙、电极损耗和加工速度等。主要针对微型方窗口的加工确定电极材料、放电间隙、加工速度等电参数,并对上述分析方法进行延伸扩展。     

月球探测技术--发展历程和特点

介绍了人类发射月球探测器进行的主要探月活动以及月球探测技术的发展和演变。分析了月球探测轨道设计与地球卫星的区别 ,给出了一些最基本的设计原则。最后 ,对探测器总体系统设计中的构型技术和各分系统的特点及其设计要求作了描述     

毛刺发生机理与形态及去除方法的探讨

文章论述了零件毛利发生的机理、毛刺的形态及因毛刺的存在而引起的产品不稳定状态。同时,介绍了机械、电解、化学、磁力等去毛刺的原理与方法,提出了去毛刺加工、检测应纳入科学化、规范化管理的设想。     

机构动态演示的制作

使用Flash软件制作机构动态演示计算机辅助教学课件 ,并能够通过按钮指令控制机构运动。说明了如何将其插入到软件FrontPage中在网上发布 ,利用此方法 ,可以制作多种网上发布的课件。     

Multi-GNSS contributions to differential code biases determination and regional ionospheric modeling in China

Due to the limited number and uneven distribution globally of Beidou Satellite System (BDS) stations, the contributions of BDS to global ionosphere modeling is still not significant. In order to give a more realistic evaluation of the ability for BDS in ionosphere monitoring and multi-GNSS contributions to the performance of Differential Code Biases (DCBs) determination and ionosphere modeling, we select 22 stations from Crustal Movement Observation Network of China (CMONOC) to assess the result of regional ionospheric model and DCBs estimates over China where the visible satellites and monitoring stations for BDS are comparable to those of GPS/GLONASS. Note that all the 22 stations can track the dual- and triple-frequency GPS, GLONASS, and BDS observations. In this study, seven solutions, i.e., GPS-only (G), GLONASS-only (R), BDS-only (C), GPS + BDS (GC), GPS + GLONASS (GR), GLONASS + BDS (RC), GPS + GLONASS + BDS (GRC), are used to test the regional ionosphere modeling over the experimental area. Moreover, the performances of them using single-frequency precise point positioning (SF-PPP) method are presented. The experimental results indicate that BDS has the same ionospheric monitoring capability as GPS and GLONASS. Meanwhile, multi-GNSS observations can significantly improve the accuracy of the regional ionospheric models compared with that of GPS-only or GLONASS-only or BDS-only, especially over the edge of the tested region which the accuracy of the model is improved by reducing the RMS of the maximum differences from 5–15 to 2–3 TECu. For satellite DCBs estimates of different systems, the accuracy of them can be improved significantly after combining different system observations, which is improved by reducing the STD of GPS satellite DCB from 0.243 to 0.213, 0.172, and 0.165 ns after adding R, C, and RC observations respectively, with an increment of about 12.3%, 29.4%, and 32.2%. The STD of GLONASS satellite DCB improved from 0.353 to 0.304, 0.271, and 0.243 ns after adding G, C, and GC observations, respectively. The STD of BDS satellite DCB reduced from 0.265 to 0.237, 0.237 and 0.229 ns with the addition of G, R and GR systems respectively, and increased by 10.6%, 10.4%, and 13.6%. From the experimental positioning result, it can be seen that the regional ionospheric models with multi-GNSS observations are better than that with a single satellite system model.