Dissipative Solitary Kinetic Alfvén Waves and Electron Acceleration in the Solar Corona

Nonthermal electrons play a major role during solar flares since not only they contain a large amount of the released energy but also they provide important information of the flaring physics through their nonthermal radiation in radio and hard X-ray bands. In a recent work Wu (Phys. Plasmas 10 (2003) 1364) proposed that dissipative solitary kinetic Alfvén wave (DSKAW) with a local shock-like structure could provide an efficient acceleration mechanism for energetic electrons in a low-β plasma. In the present paper dynamical characteristics of the DSKAW acceleration mechanism in solar coronal plasmas are studied and its application to the acceleration of flaring electrons is discussed.     

圆锥激波的反解法

给出了超音速圆锥激波的一种反解法，该方法由假定的激波处向锥面推算，具有计算效率高，适于计算机处理等特点。     

一类导弹控制系统的模态解耦

本文研究非旋转式导弹控制系统的模态解耦能力。证明了具有俯仰、偏航和滚动三个控制通道的控制系统可以实现俯仰、偏航两种运动模态对滚动运动模态的完全解耦。给出了模态解耦控制系统的设计方法。对一种导弹控制系统进行了验证性设计,做了数字仿真。     

有控飞行力学在无人飞行器研制和使用中的作用

本文从工程实践观点出发，结合无人飞行器，特别是战术导弹和制导兵器的特点，扼要讨论了与此密切相关的有控习行力学研究工作的某些进展情况，文中将有控习行力学问题分为两大类，即典型的飞行力学问题和相关的飞行力学问题，强调了多学科交 对飞行力学研究的重要意义；同时，还指出了有控飞行力学在未来軎与研制和使用中的作用。     

飞行器合理传递参数的解法

本文基于矢量矩阵分析法,建立了含气动、结构和飞行参数及其偏量的数学模型,它可用来分析飞行器的合理传递参数。按此方法不仅可以同时调整若干设计参数,而且还可简化计算机辅助设计的程序。为选择合理传递参数,列出了设计参数的调整准则。 取用动态因子和转换因子,使所得方法对于正常式、鸭式、旋转弹翼式和弹道式导弹都是适用的。     

子午面内Alfvén波的传播特征

本文使用由ＷＫＢ近似得到的Ａｌｆｖｅｎ波传播的张量表达式,具体计算和讨论了一种太阳子午面内含盔形－电流片磁位形的流场中Ａｌｆｖｅｎ波的传播特征,主要结果是：（１）Ａｌｆｖｅｎ波磁场起伏随日心距离的增加而衰减,其中极开区的衰减远快于赤道区,但随着距离的增大,这种纬度关系将迅速变弱,以致在较远空间,磁起伏相差很小,衰减很慢;（２）Ａｌｆｖｅｎ波的相对磁场起伏ｂ／Ｂ随着距离的增加而迅速增大,在几个太阳半径之后变化不再明显,达到所谓的＂饱和＂;在大日心距离的盔形电流片附近,Ａｌｆｖｅｎ波将成为重要的磁场组成部分;（３）Ａｌｆｖｅｎ波速度起伏纬度关系较为明显,相对速度起伏。ｕ／Ｕ随着距离增大而衰减,电流片区衰减得较快,但这种纬度差别将变弱．与黄道面内Ａｌｆｖｅｎ波传播特征的具体比较表明,磁场涨落的变化特征与背景场位形存在着十分密切的关系,但速度涨落与背景场没有这种明显关系．     

电磁场对航空电子设备干扰的预测研究

论述飞机内部辐射电磁通过电缆线感应耦合，形成对电子设备干扰的机理，分析这种干扰模式既有辐射，又有传导的复合特点。应用孔缝衍射、场对线激励、含分布源传输线和网络分析等理论与方法，逐层剖析描述了预测数学模型，并给出了能够对电子设备电子元件级进行可靠性和安全性评估的实用预测软件。     

紧缩平面场扫描架系统研制

紧缩平面场(CATR)是在较小的微波暗室里模拟远场的电磁环境,以行进各种天线的测量和研究.其最终性能指标要由紧缩平面场扫描架评定.根据紧缩平面场扫描测量原理,及其对扫描架平面度、直线度、定位精度及自动化程度的要求,研制了极坐标型紧缩场扫描架系统,通过采用高精度直线导轨、平面度微调方式和基于工业控制计算机的数字控制技术,达到了所要求的检测精度,满足了紧缩平面场扫描测量的要求.     

A possible flyby anomaly for Juno at Jupiter

In the last decades there have been an increasing interest in improving the accuracy of spacecraft navigation and trajectory data. In the course of this plan some anomalies have been found that cannot, in principle, be explained in the context of the most accurate orbital models including all known effects from classical dynamics and general relativity. Of particular interest for its puzzling nature, and the lack of any accepted explanation for the moment, is the flyby anomaly discovered in some spacecraft flybys of the Earth over the course of twenty years. This anomaly manifest itself as the impossibility of matching the pre and post-encounter Doppler tracking and ranging data within a single orbit but, on the contrary, a difference of a few mm/s in the asymptotic velocities is required to perform the fitting.Nevertheless, no dedicated missions have been carried out to elucidate the origin of this phenomenon with the objective either of revising our understanding of gravity or to improve the accuracy of spacecraft Doppler tracking by revealing a conventional origin.With the occasion of the Juno mission arrival at Jupiter and the close flybys of this planet, that are currently been performed, we have developed an orbital model suited to the time window close to the perijove. This model shows that an anomalous acceleration of a few mm/s² is also present in this case. The chance for overlooked conventional or possible unconventional explanations is discussed.     

直升机机内PWM照明调光系统产生音频干扰问题的研究

在直升机机内照明调光领域，国外军机已广泛采用脉冲宽度调制（PWM）调光方式。PWM调光方式相比传统线性调光方式具有以下明显优点：效率高，调光范围宽，功耗小，带载能力强，附加损耗小等。但PWM调光系统的不足是电磁辐射，尤其会对机内通话系统产生音频干扰，在机通耳机中会出现明显干扰声，影响机内通话质量。本方案能有效抑制PWM...