步进电机在真空低温下的驱动特性分析

文章对步进电机的特点、应用情况及误差补偿处理进行了分析,并提出了在真空低温环境下,除了按常规计算外还必须进行超常力矩试验。     

水系统装置扬程的计算及泵的选型分析

为了提高水系统中水泵的实际运行效率和扬程利用率,降低发动机试验成本,减少能量浪费,以某型发动机台架试验水系统为研究对象,综合考虑了装置静扬程、管路的各种局部损失和沿程损失开展装置扬程的计算。同时根据水系统所需的装置扬程、流量及其变化规律,从泵的参数及其特性曲线入手,进行泵的选型分析,确定合适的泵的类型、台数及连接方式。通过水系统装置扬程的计算和泵的选型分析,结合泵带来的能效利用、工程投入和运行费用等因素,可在满足发动机试验需要的同时实现经济利益最大化,为今后类似水系统工程的设计提供借鉴和指导。     

NASA月球激光通信演示验证试验

为满足日益增长的大数据量、高数据速率传输要求,NASA(National Aeronautics and Space Administration,美国国家航空航天局)正开启采用激光技术进行空间通信的新时代,并于近年相继开展了多项自由空间激光通信技术研究项目。针对该情况,重点介绍LLCD(Lunar Laser Communications Demonstration,月球激光通信演示验证)项目的系统组成和工作状况:该项目由NASA实施,首次采用激光作为载波在绕月飞行器和地面接收机之间进行双向激光通信,通过飞行演示验证了下行速率为622 Mbit/s和上行速率为20 Mbit/s的月地双向空间激光通信,以及端到端DTN(Delay Tolerant Networking,容延迟网络)数据传输,并验证了作为激光通信链路副产品的高精度测距技术,试验成果超出预期。最后展望LLCD后续发展,供我国相关研究工作参考借鉴。     

自整角机/数字转换器及其应用

介绍了ZSZ系列自整角机／数字转换器的结构，特性和工作原理，以及转换器在实际应用中的接口电路。     

斯特林制冷机真空环境模拟试验

文章针对空间红外遥感器应用特点,进行了斯特林制冷机的模拟真空环境试验。试验结果表明:温度环境和导热条件是影响斯特林制冷机空间应用的重要因素。     

自旋火箭姿态运动的稳定性分析和数学仿真

本文主要对自旋火箭姿态运动的稳定性进行了分析,并给出了数学仿真结果。飞行试验结果表明,稳定性分析和数学仿真是正确、可靠的。     

ADμC824在温度测控方面的应用

介绍了ADμC824的部分特性及其在精确控温方面的软硬件设计思路。     

Simulation and analysis of chemical release in the ionosphere

Ionospheric inhomogeneous plasma produced by single point chemical release has simple space-time structure, and cannot impact radio wave frequencies higher than Very High Frequency (VHF) band. In order to produce more complicated ionospheric plasma perturbation structure and trigger instabilities phenomena, multiple-point chemical release scheme is presented in this paper. The effects of chemical release on low latitude ionospheric plasma are estimated by linear instability growth rate theory that high growth rate represents high irregularities, ionospheric scintillation occurrence probability and high scintillation intension in scintillation duration. The amplitude scintillations and the phase scintillations of 150?MHz, 400?MHz, and 1000?MHz are calculated based on the theory of multiple phase screen (MPS), when they propagate through the disturbed area.     

Orbit determination of BDS-3 satellite based on regional ground tracking station and inter-satellite link observations

The BeiDou global navigation satellite system (BDS-3) has established the Ka-band inter-satellite link (ISL) to realize a two-way ranging function between satellites, which provides a new observation technology for the orbit determination of BDS-3 satellites. Therefore, this study presents a BDS satellite orbit determination model based on ground tracking station (GTS) observations and ISL ranging observations firstly to analyze the impact of the ISL ranging observations on the orbit determination of BDS-3 satellites. Subsequently, considering the data fusion processing, the variance component estimation (VCE) algorithm is applied to the parameter estimation process of the satellite orbit determination. Finally, using the measured data from China’s regional GTS observations and BDS-3 ISL ranging observations, the effects of ISL ranging observations on the orbit determination accuracy of BDS-3 satellites are analyzed. Moreover, the impact of the VCE algorithm on the fusion data processing is evaluated from the aspects of orbit determination accuracy, Ka-band hardware delay parameter stability, and ISL ranging observation residuals. The results show that for China’s regional GTSs, the addition of BDS-3 ISL ranging observations can significantly improve the orbit determination accuracy of BDS-3 satellites. The observed orbit determination accuracy of satellite radial component is improved from 48 cm to 4.1 cm. In addition, when the initial weight ratio between GTS observations and ISL ranging observations is not appropriate, the various indicators which include orbit determination accuracy, ISL hardware delay, and ISL observation residuals were observed to have improved after the adjustment of the VCE algorithm. These results validate the effectiveness of the VCE algorithm for the fusion data processing of the GTS observations and ISL ranging observations.     

一种GPS抗干扰及干扰DOA估计工程集成方法

卫星导航干扰对消技术和干扰测向技术是卫星导航干扰对抗的两个典型方向,并逐渐成为当前卫星导航抗干扰装备的标配功能。如何实现干扰对消和干扰测向的高效集成成为制约工程实现的主要瓶颈之一。提出一种GPS抗干扰及DOA估计的工程集成方法,通过优化噪声子空间估计工程实现,实现了高性能抗干扰和高精度干扰测向的高效集成,与抗干扰模块和干扰测向模块相比,集成模块极大降低了工程实现资源。测试结果表明该方法可以有效对抗干信比60dB的干扰,并提供2度的测向精度。