H∞控制及其应用

本文叙述了Ｈ∞控制器设计的频域法和代数法，在频哉法中介绍了标准问题的模型匹配解法和丁谱分解法；在代数法中介绍了多项式法，直接状态空间法，最后简述了几个实际应用的例子。     

Reconstructed 3-d magnetic field structure and hard X-ray two ribbons for 2000 Bastille-day event

The Bastille-day event in 2000 produced energetic 3B/X5.6 flare with a halo CME, which had great geo-effects consequently. This event has been studied extensively and it is considered that it follows the two-ribbon flare model. The flare/CME event was triggered by an erupting filament and TRACE observations showed formation of giant arcade structures during the flare process. Hard X-ray (HXR) two ribbons revealed for the first time in this flare event (Masuda et al., 2001). The reconstruction of 3-D coronal magnetic fields revealed a magnetic flux rope structure, for the first time, from extrapolation of observed photospheric vector magnetogram data and the flux rope structure was co-spatial with portion of the filament and a UV bright lane (Yan et al., 2001a, 2001b). Here we review some recent work related to the flux rope structure and the HXR two ribbons by comparing their locations and the flux temporal profiles during the flare process so as to understand the energy release and particle accelerations. It is proposed that the rope instability may have triggered the flare event, and reconnection may occur during this process. The drifting pulsation structure in the decimetric frequency range is considered to manifest the rope ejection, or the initial phase of the coronal mass ejection. The HXR two ribbons were distributed along the flux rope and the rope foot points coincide with HXR sources. The energy dissipation from IPS observations occurred within about 100 R _⋅ is consistent with the estimate for the flux rope system. This revised version was published online in August 2006 with corrections to the Cover Date.     

卫星交会的自主导航技术

论述卫星交会自主导航的飞行任务背景和概念 ,综述国内外学者正在进行探索研究的思路 ,以期引起国内学者的的注意、探讨和深入研究。     

谈合并会计报表抵销分录的编制

本文详细介绍了为何要编制合并会计报表,哪些应纳入合并会计报表范围,在公司连续编制情况下, 对以前年度已做抵销的事项在今后编制合并会计报表时为何还要进行抵销进行了论述。     

悬筐式蒸发器的结构设计

本文从设计角度对悬筐式蒸发器的结构进行了介绍和总结,并提出了一些结构的改进意见。     

载人航天可靠性与空间环境试验

文章通过对国外载人航天事故统计,分析各种空间环境条件对航天器及航天员的影响,阐述了空间环境试验对提高载人航天可靠性的重要意义,提出为了提高载人航天的可靠性,应进行充分和严格的空间环境模拟试验。     

一种具有较强泛化能力的神经网络模型研究与应用

分析了影响神经网络模型泛化能力的因素。以电解铝过程中氧化铝浓度的神经网络软测量为例 ,提出了利用先验知识确定网络结构 ,采用特定实验保证样本数量和质量 ,离线训练加在线学习修正模型等措施 ,改善神经网络模型的泛化能力。现场应用表明这些措施是有效的。这样建立的神经网络模型准确 ,泛化能力强 ,为实现过程的先进控制提供了可靠保障     

用Visual FoxPro进行动态界面的设计

本文介绍用 Visual FoxPro的定时器。标签、按钮等控件和控件的属性、方法、事件等在界面上设计动态字幕、动态按钮等若干动态效果的方法。     

振动对空间光通信系统误码率影响的分析

在空间光通信系统中，由于卫星平台的振动，使得光发射机发生振动，从而对通信系统的误码率产生影响，本文针对光射光束为高斯光束时，振动对误码率的影响问题进行研究。结果表明，在振动时不仅振幅影响着误码率，而且波长也对误码率有影响，但通信距离对误码率的影响不大，一般可以忽略。     

求解装箱问题的遗传算法

本文提出了两种求解装箱问题（ＢｉｎＰａｃｋｉｎｇ）的遗传算法。一种是简单遗传算法,它采用等长度字符代码编码方法,使用常规的遗传操作算子。另一种是混合遗传算法,它综合运用解装箱问题的ＦＦＤ（ＦｉｒｓｔＦｉｔＤｅ－ｃｒｅａｓｉｎｇ）近似算法和简单遗传算法。试算结果表明,由这两种遗传算法所得到的装箱方案较一些近似算法所得到的装箱方案都要好。