车载遥测站天线标校复查中存在的问题及对策

车载遥测跟踪站天线展开后,需要进行远场标校复查。由于受标校距离、天线仰角以及周围环境等各种条件的限制,使得主天线、引导天线的光电轴匹配检查难以保证精度要求,从而影响跟踪性能。针对这些问题,本文提出在近场条件下直接悬挂信标机进行标校复查,以保证光电轴匹配精度。并针对YQ- 312 S频段遥测跟踪车载站的实际推出角度转换公式。最后给出实例     

Statistical characteristics of locally generated ESF during equinoctial months over Sanya

Understanding the local generation rate of equatorial spread-F (ESF) is important for forecasting ionospheric scintillation. Using the GPS ionospheric scintillation/TEC and VHF radar data during March-April and September-October from 2010 to 2014, the occurrence of ionospheric scintillation, TEC fast fluctuation, and backscatter plume were studied. Through analyzing the simultaneous occurrence of ionospheric scintillation, TEC fast fluctuation and backscatter plume, the local generation rate of ESF over Sanya was investigated. The results show that the monthly generation rate varies between 0% and 68%. A significant equinoctial asymmetry of local generation rate of ESF can be found in 2010, 2013 and 2014. The local generation rate of ESF increases from 2010 to 2014 during March-April, while it does not have similar trend during September-October. The plasma vertical drift influenced by solar activity has a significant impact on the monthly generation rate. The equinoctial asymmetry of plasma vertical drift may contribute a lot to the equinoctial asymmetry of the generation rate of ESF.     

分区并行跨声速流的计算

本文采用求解Ｎ－Ｓ方程方法计算了轴对称钝头倒锥体外形的跨声速大迎角层流流动。     

基于功率裕度的某型发动机全寿命性能研究

随着使用时间不断增加,研究飞行队所有选装ARRIEL2S系列发动机全寿命性能变化趋势的必要性突显.针对SRRIEL2S系列发动机全寿命性能参数变化特点,提出使用基于可几误差舍弃理论处理发动机功率校验数据,分区间描绘该系发动机全寿命性能指标变化趋势,给出该系发动机全寿命性能特点,为机务工程人员监控该系发动机提供有利依据；提出延长功率校验间隔的假设,并在理论上做了充分论证,为节约该系发动机运行成本提供一个明确及可行的方向.     

MANEUVERING TARGET TRACKING USING FUZZY COMPENSATOR

Ｔｈｅｍａｎｅｕｖｅｒｉｎｇｔａｒｇｅｔｓｔｒａｊｅｃｔｏｒｙｅｓｔｉｍａｔｉｏｎｐｒｏｂｌｅｍｈａｓｂｅｎａｎｉｍｐｏｒｔａｎｔｔｏｐｉｃａｎｄｍａｎｙｆｒｕｉｔｆｕｌｒｅｓｕｌｔｓｈａｖｅｂｅｅｎａｔａｉｎｅｄ．Ｉｔｉｓｂｏｔｈｔｈｅｋｅｙａｎ...     

基于构型管理的飞机技术出版物数据结构研究

在飞机复杂产品的整体结构基础上,依据S1000D规范,采用模块化技术,建立技术出版物的三层数据结构,保证数据的重用性和一致性,便于技术出版物的构型控制管理。     

连接参数对Ti53311S 高温钛合金TLP 连接接头性能的影响

采用Cu作为中间层实现了Ti53311S合金的TLP连接,通过SEM、EDS方法分析了接头界面的微观组织,研究了接头界面微观组织及力学性能随TLP连接温度及保温时间的变化规律。结果表明:TLP连接接头的典型界面结构为Ti53311S/β-Ti/Ti、Cu(Sn)金属间化合物/β-Ti/Ti53311S。随着TLP连接温度的升高或保温时间的增加,焊缝宽度逐渐增加,Cu元素向母材侧的扩散程度更加充分,化合物相分解消失,接头室温抗拉强度先大幅升高后趋于稳定,连接工艺为980℃/20 min时,接头抗拉强度达到最大值899 MPa。     

多喷口环量控制翼型流动的研究

提出了多喷口环量控制翼型的想法，并进行了数值研究。结果表明，多喷口环量控制方法可以在中、小Ｃμ吹气时提高翼型的升力和减小能耗，并能改善环量控制翼型在较高来流马赫数下的气动性能，避免“压缩性失速”。     

S5 0716+714: GeV variability study

The GeV observations by Fermi-LAT give us the opportunity to characterize the high-energy emission (100 MeV–300 GeV) variability properties of the BL Lac object S5 0716+714. In this study, we performed flux and spectral analysis of more than 3 year long (August 2008 to April 2012) Fermi-LAT data of the source. During this period, the source exhibits two different modes of flux variability with characteristic timescales of ∼75 and ∼140 days, respectively. We also notice that the flux variations are characterized by a weak spectral hardening. The GeV spectrum of the source shows a clear deviation from a simple power law, and is better explained by a broken power law. Similar to other bright Fermi blazars, the break energy does not vary with the source flux during the different activity states. We discuss several possible scenarios to explain the observed spectral break.     

飞机结构修理手册编制研究

首先介绍了飞机结构修理手册的编制要求和编制依据,其次分别阐述了依据ATA2200和S1000D标准进行飞机结构修理手册编写的方法,最后比较两种标准的特点,并对大型客机结构修理手册的编制工作提出了初步建议。