直9直升机机载数据传输电缆电磁耦合分析

通过对数据传输电缆的仿真分析计算,得到了传输信号频率、电缆回路之间的距离与电磁耦合之间的关系.对于直9系列直升机中数据传输电缆的物理模型计算结果表明,感应电压会在传输频率为75MHz时达到最大值,线间距离为1.5mm时具有最小值.分析结果为直9系列直升机/飞机机载数据电缆的布线优化和电磁兼容改进设计提供一定参考依据.     

基于P89C51X2BA单片机实现智能程控数字相位变换器设计

数字相位变换器在电子系统中的应用比较广泛,普通的数字相位变换器均由硬件电路搭接而成,系统复杂,故障率高。本文介绍了一种基于单片机控制的智能数字相位变换器的构建,弥补了普通的数字相位变换器的不足。以P89C51X2BA和逻辑门电路为基础,阐释了实现的原理和方法,给出了系统结构和软硬件构成。     

X波段波导端头裂缝的互耦分析

用矩量法(MOM)导出求解X波段波导端头裂缝单元间互耦等效磁流的模型。在此基础上给出了等效磁流在激励和未激励单元内部产生的场、反射系数、驻波系数和两单元间耦合系数等的计算公式。分别在共E、H面条件下分析了两X波段波导端头裂缝互耦的影响,并对单元间不同相对距离和工作频率时的互耦影响规律进行了讨论。研究结果表明,该算法简单,计算值与测试结果吻合较好。     

脉宽调制器中一类振荡器的全面解析结果

用分析法全面讨论脉宽调制器（IC：1842/3/4/5,1842A/3A/4A/5A）中振荡器的振荡特征参数（占空比D和频率f）与外接电阻R和电容C的关系.我们得到以R、C为自变量表达D和f的函数,以D、f为自变量求R、C的函数.并根据这些函数的计算结果绘制描述D、f、R、C（1F）4个参数之间的关系曲线.这些结果,不仅提升了对这类振荡器的认知,而且可供设计时直接引用和参考.     

面心立方合金调幅分解与有序化的X射线和透射电镜衍射研究

在点阵波理论基础上，通过假定合金中溶质原子浓度的适当分布并建立与之相应的衍射波波幅表达式，利用计算机模拟得面心立方（Ｃｕ－４ｗ ｔ％ Ｔｉ）合金调幅（Ｓｐｉｎｏｄａｌ）分解与有序化共存的Ｘ射线衍射边带形貌，其波形与实验结果颇为相近。进一步根据迭加原理在两相互垂直方向上对上述衍射边带合成，所得有序化模拟衍射花样与电镜衍射谱完全一致     

The Coma of Comet 9P/Tempel 1

As comet 9P/Tempel 1 approaches the Sun in 2004–2005, a temporary atmosphere, or “coma,” will form, composed of molecules and dust expelled from the nucleus as its component icy volatiles sublimate. Driven mainly by water ice sublimation at surface temperatures T > 200 K, this coma is a gravitationally unbound atmosphere in free adiabatic expansion. Near the nucleus (≤ 10² km), it is in collisional equilibrium, at larger distances (≥10⁴ km) it is in free molecular flow. Ultimately the coma components are swept into the comet’s plasma and dust tails or simply dissipate into interplanetary space. Clues to the nature of the cometary nucleus are contained in the chemistry and physics of the coma, as well as with its variability with time, orbital position, and heliocentric distance. The DI instrument payload includes CCD cameras with broadband filters covering the optical spectrum, allowing for sensitive measurement of dust in the comet’s coma, and a number of narrowband filters for studying the spatial distribution of several gas species. DI also carries the first near-infrared spectrometer to a comet flyby since the VEGA mission to Halley in 1986. This spectrograph will allow detection of gas emission lines from the coma in unprecedented detail. Here we discuss the current state of understanding of the 9P/Tempel 1 coma, our expectations for the measurements DI will obtain, and the predicted hazards that the coma presents for the spacecraft. An erratum to this article is available at .     

Deep Impact Mission Design

The Deep Impact mission is designed to provide the first opportunity to probe below the surface of a comet nucleus by a high-speed impact. This requires finding a suitable comet with launch and encounter conditions that allow a meaningful scientific experiment. The overall design requires the consideration of many factors ranging from environmental characteristics of the comet (nucleus size, dust levels, etc.), to launch dates fitting within the NASA Discovery program opportunities, to launch vehicle capability for a large impactor, to the observational conditions for the two approaching spacecraft and for telescopes on Earth.     

The History and Dynamics of Comet 9P/Tempel 1

Since its discovery in 1867, periodic comet 9P/Tempel 1 has been observed at 10 returns to perihelion, including all its returns since 1967. The observations for the seven apparitions beginning in 1967 have been fit with an orbit that includes only radial and transverse nongravitational accelerations that model the rocket-like thrusting introduced by the outgassing of the cometary nucleus. The successful nongravitational acceleration model did not assume any change in the comet’s ability to outgas from one apparition to the next and the outgassing was assumed to reach a maximum at perihelion. The success of this model over the 1967–2003 interval suggests that the comet’s spin axis is currently stable. Rough calculations suggest that the collision of the impactor released by the Deep Impact spacecraft will not provide a noticeable perturbation on the comet’s orbit nor will any new vent that is opened as a result of the impact provide a noticeable change in the comet’s nongravitational acceleration history. The observing geometries prior to, and during, the impact will allow extensive Earth based observations to complement the in situ observations from the impactor and flyby spacecraft.     

九自由度运动模拟器相对位置精度分析与指标分解

摘要： 九自由度运动模拟器是标定航天器交会对接GNC子系统中交会对接光学成像敏感器（CRDS）的关键设备,具有较高的相对位置精度要求.以此为出发点,对影响系统综合指标的误差组成进行系统性分析.梳理各误差分量的关系及相互作用原理,建立误差模型,通过对系统综合指标进行合理的分解与分配,最终使九自由度运动模拟器系统精度达到设计要求.     

X波段遥感数传微波通道

遥感数传微波通道是数传遥感卫星的发射系统,是实现地物信息实时传输的重要设备。为了实现高码速率的传输,分别利用上边带上变频器和下边带上变频器将传输的微波信道分成两个信道,每个信道传输53Mbit/s,两个信道可传输的码速率为106Mbit/s。文章介绍了单信道微波通道和双信道微波通道,并扼要地介绍了微波通道中的上变频器和阶跃管电抗开关倍频器。