QX-1 GNOS M掩星数据质量分析

QX-1 GNOS M是首台在轨实现北斗、GPS和Galileo三系统兼容的小型商业化全球导航卫星掩星探测仪. 2021年10月14日18:51 LT, 气象一号(QX-1)卫星发射并入轨. 自发射以来, 该卫星已收集大量观测数据. 基于QX-1 GNOS M的结构组成及性能, 统计分析了2022年8月17日全天的掩星事件及其全球分布情况. 通过将8月17日至9月3日的掩星数据与NCEP再分析模式对比, 评估QX-1掩星事件的探测穿透深度和折射率精度, 同时检验Galileo掩星数据的可靠性和一致性. 初步分析结果表明, QX-1 GNOS M在实现三系统兼容后, 掩星事件数量相较于仅使用GPS系统的情况增加了约1.5倍. 这一结果进一步证明, 不同全球导航卫星系统(GNSS)所提供的掩星数据在精度上具有一致性. 此外研究显示, 在多系统兼容的背景下, QX-1 GNOS M能够提供更为丰富和精确的气象数据.     

电波折射误差的经验-分层修正算法

建立了一种新的电波折射修正算法——经验-分层电波折射修正算法。经过与电波折射误差的经验修正和分层实测指数修正方法修正效果的比较，证实了该算法效果接近分层实测指数修正方法，明显优于经验修正方法。该方法为一些不其备提供分层电波折射参数的航天测控站电波折射误差修正问题，提供了行之有效的技术手段，对航天测控工程具有应用价值。     

PCM/DPSK遥测信号的全软化解调方法

研究了 PCM/ DPSK遥测信号的全软化解调原理 ,对其算法进行了理论设计 ,并在此基础上进行软件设计 ,完成了数字下变频、滤波抽取、定时误差提取、内插法码同步和差分判决的全软件化实现     

机载GNSS掩星观测反演大气折射率廓线研究

作为星载掩星技术的推广,基于飞机平台的无线电掩星技术备受关注。为了将机栽掩星技术更好地应用到工程实践中,文章通过介绍机载掩星探测的基本原理和主要特点、模拟仿真,对机载掩星的反演算法进行了探讨,并给出模拟结果：包括利用STK仿真软件生成仿真场景;采用3维射线追踪技术模拟机载无线电掩星,预报掩星事件出现的时间、仰角,模拟信号传播特征;详细研究大气层内折射率反演技术并给出反演结果。研究结果表明,模拟仿真对机载掩星工程化实现是有益的。最后展望了机载掩星探测的发展趋势,提出了弱掩星信号的捕获跟踪、飞机平台的精度定位测速以及反射信号的抗干扰三项技术及工程化中需解决的技术难点。     

Heliospheric asymmetries due to the action of the interstellar magnetic field

We discuss the asymmetry of the heliospheric discontinuities obtained from the analysis of 3D modeling of the solar wind (SW) interaction with local interstellar medium (LISM). The flow of charged particles is governed by the ideal MHD equations and the flow of neutral particles is described by the Boltzmann equation. The emphasis is made on the asymmetries of the termination shock (TS) and the heliopause under the combined action of the interstellar and interplanetary magnetic fields (ISMF and IMF) in the presence of neutral hydrogen atoms whose transport through the heliosphere is modeled kinetically, using a Monte Carlo approach. We show that the deflection of neutral hydrogen flow from its original direction in the unperturbed LISM is highly anisotropic and evaluate a possible angle between the hydrogen deflection plane measured in the SOHO SWAN experiment and the plane containing the ISMF and LISM velocity vectors for different ISMF strengths. It is shown that the ISMF of a strength greater than 4 μG can account for the 10 AU difference in the TS heliocentric difference observed during its crossing by the Voyager 1 and Voyager 2 spacecraft, which however results in a larger discrepancy between the calculated and observed velocity distributions. The effect of a strong ISMF on the distribution of plasma quantities in the inner heliosheath and on 2–3 kHz radio emission is discussed.     

Relativistic jets from black hole binaries

Relativistic jets are now believed to be a fairly ubiquitous property of accreting compact objects, and are intimately coupled with the accretion history. Associated with rapid changes in the accretion states of the binary systems, ejections of relativistic plasma can be observed at radio frequencies on timescale of weeks before becoming undetectable. However, recent observations point to long term effects of these ejecta on the interstellar medium with the formation of large scale relativistic jets around binary systems.     

VXI总线在FY-2卫星无线测试中的应用

介绍了风云二号(FY-2)气象卫星VXI总线无线测试系统的功能、硬/软件结构.给出了设计中采用的VXI总线技术、硬件配置和在LabWindows/CVI环境中的软件模块化设计方案,以及输出功率限制、微波开关初始化控制、系统安全管理控制和仪器控制顺序正确等软件安全性和可靠性设计.该测试系统的测试能力强、体积小、研制成本低,具有测试结果准确、自动化程度高、工作稳定可靠、操作简便,以及转移和维护容易等优点,在FY-2卫星电性星、正样星和发射星测试中发挥了重要作用.