Occurrence features of simultaneous H+- and He+-band EMIC emissions in the outer radiation belt

As an important loss mechanism of radiation belt electrons, electromagnetic ion cyclotron (EMIC) waves show up as three distinct frequency bands below the hydrogen (H⁺), helium (He⁺), and oxygen (O⁺) ion gyrofrequencies. Compared to O⁺-band EMIC waves, H⁺- and He⁺-band emissions generally occur more frequently and result in more efficient scattering removal of <～5?MeV relativistic electrons. Therefore, knowledge about the occurrence of these two bands is important for understanding the evolution of the relativistic electron population. To evaluate the occurrence pattern and wave properties of H⁺- and He⁺-band EMIC waves when they occur concurrently, we investigate 64 events of multi-band EMIC emissions identified from high quality Van Allen Probes wave data. Our quantitative results demonstrate a strong occurrence dependence of the multi-band EMIC emissions on magnetic local time (MLT) and L-shell to mainly concentrate on the dayside region of L?=?～4–6. We also find that the average magnetic field amplitude of H⁺-band waves is larger than that of He⁺-band waves only when L?<?4.5 and AE¹?<?300?nT, and He⁺-band emissions are more intense under all other conditions. In contrast to 5 events that have average H⁺-band amplitude over 2 nT, 19 events exhibit >2 nT He⁺-band amplitude, indicating that the He⁺-band waves can be more easily amplified than the H⁺-band waves under the same circumstances. For simultaneous occurrences of the two EMIC wave bands, their frequencies vary with L-shell and geomagnetic activity: the peak wave frequency of H⁺-band emissions varies between 0.25 and 0.8 f_cp with the average between 0.25 and 0.6 f_cp, while that of He⁺-band emissions varies between 0.03 and 0.23 f_cp with the average between 0.05 and 0.15 f_cp. These newly observed occurrence features of simultaneous H⁺- and He⁺-band EMIC emissions provide improved information to quantify the overall contribution of multi-band EMIC waves to the loss processes of radiation belt electrons.     

Detection of the quantity of kinesin and microgravity-sensitive kinesin genes in rat bone marrow stromal cells grown in a simulated microgravity environment

Kinesin and kinesin-like proteins (KLPs) constitute a superfamily of microtubule motor proteins found in all eukaryotic organisms. Members of the kinesin superfamily are known to play important roles in many fundamental cellular and developmental processes. To date, few published studies have reported on the effects of microgravity on kinesin expression. In this paper, we describe the expression pattern and microgravity-sensitive genes of kinesin in rat bone marrow stromal cells cultured in a ground-based rotating bioreactor. The quantity of kinesin under the clinorotation condition was examined by immunoblot analysis with anti-kinesin. Furthermore, the distribution of kinesin at various times during clinorotation was determined by dual immunostaining, using anti-kinesin monoclonal antibody or anti-β-tubulin monoclonal antibody. In terms of kinesin quantity, we found that the ratios of the amounts of clinorotated/stationary KLPs decreased from clinorotation day 5 to day 10, although it increased on days 2 and 3. Immunofluorescence analysis revealed that kinesin in the nucleus was the first to be affected by simulated microgravity, following the kinesin at the periphery that was affected at various times during clinorotation. Real-time RT-PCR analysis of kinesin mRNA expression was performed and led to the identification of 3 microgravity-sensitive kinesin genes: KIF9, KIFC1, and KIF21A. Our results suggest that kinesin has a distinct expression pattern, and the identification of microgravity-sensitive kinesin genes offers insight into fundamental cell biology.     

雷达波形的水印技术

提出了一种抗有源欺骗干扰的新技术——雷达波形的水印技术。常规雷达波形易被干扰机截获并被分析出信号参数。若限定相位变化范围,按调整后的波形与原波形相关性最小的原则对原波形进行相位优化调整,在调整范围较小的情况下,干扰机一般并不能察觉出这种变化。雷达对相位调整后的波形用加权失配滤波器进行脉压,真正的目标没有损失,而对干扰机辐射的原波形却不能形成相关峰,这样,雷达就能自动地抑制欺骗式干扰形成的假目标。将这种具有防伪且保护雷达能正常检测目标功能的相位调整技术称为雷达波形的水印技术,所得的波形称为水印雷达波形。仿真结果证明了此方法的有效性。     

位置伺服滑态控制系统的单片机实现

本文以MCS-51(8031)为基础研究了位置伺服的滑态控制(Sliding Mode Control,简称为SMC)系统的实现。提出了SMC律的设计方法,给出了8031 SMC控制器的硬软件的设计方法与技巧,并在8031 SMC控制器上作了模数混合仿真,给出了仿真结果。     

鲁棒调节器设计及其在飞行控制系统中的应用

本文提出一种降低参数灵敏度的鲁棒调节器设计法。它根据灵敏度指标的要求，利用最优调节器的性质设计了状态反馈调节器，所构成的系统具有良好的参数鲁棒性和动态特性。该方法计算简单，实现方便。文中给出了在飞行控制系统中的应用实例。     

复合陶瓷天线罩表面防潮性能的研究

通过对复合陶瓷天线罩吸潮机理进行仔细的分析,将某树脂进行改性后,采用真空浸涂和真空固化的工艺方法,显著提高天线罩的防潮性能,达到设计要求,成功运用于型号生产。     

遥测电池自动检测装置设计

介绍运用计算机检测和控制技术的遥测电池的自动检测装置,及其主要功能、硬件结构及软件流程,简述设计中所采用的关键技术。     

叶盘结构特征设计的并行方法研究

以高推比航空燃气涡轮发动机压气机部件中的新结构－－叶盘为对象，探索了基于并行工程的产品设计关键技术；考虑设计、分析和工艺等要求的特征建模方法。在微机ＣＡＤ平台初步实现了叶盘统一建模，设计约束检查。并进行了设计模型与有限元计算模型的数据传输，完成了整体叶盘的基本强度和振型分析。     

某型飞机飞参接口板的工作机理及故障模式分析

分析了某型飞机的飞参接口板工作机理 ,给出了详细的故障树和排故方法 ,可为飞参地面站人员排除飞参疑难故障和飞参地面站的国产化提供参考     

最大应变记忆元件

 本文介绍的新型的应变测试元件——最大应变记忆元件,具有记忆构件上曾经历过的最大应变值的功能。在不跟踪测量的情况下,可以得知构件上曾经历过的最大应变值,使用方便,灵敏度高。