EUV emission from normal galaxies

Using data from the Wide Field Camera EUV all-sky survey, we have established upper limits to the EUV flux from a sample of 30 bright, nearby, non-active spiral galaxies. These galaxies were chosen to be those most likely to be detected in the EUV on the basis of (i) low interstellar absorption within our own galaxy, (ii) brightness in other wavebands, (iii) high star formation activity, and (iv) proximity. The derived EUV upper limits are restrictive, and establish for the first time that the EUV flux escaping from galaxies does not constitute a major component of their bolometric luminosity, and in particular that it cannot be the sink for the energy injected into the interstellar medium by supernova explosions, as had been suggested following the failure to detect this power in the X-ray band.     

A bistatic SAR mission for earth observation based on a small satellite

The authors present a new scientific space mission consisting of a satellite carrying a receiving- only SAR which receives the signal transmitted by the ENVISAT-1 SAR. The integration of ENVISAT-1 SAR and bistatic radar data offers an improved potentiality of surface classification, three-dimensional observation, and the opportunity of advanced scientific experiments in the field of bistatic scattering. The small satellite nominal orbit and the attitude manoeuvres are designed in order to maintain an adequate overlap between the two radar swaths along the whole orbit, taking into account the ENVISAT-1 attitude and pointing. A preliminary satellite design (2-year lifetime) is then performed to evaluate the orbit decay and to determine the appropriate orbit manoeuvres (every 4 days) to control the satellites relative phase. The numerical simulation shows that a spacecraft of about 584kg is able to meet the mission requirements.     

金融工程对我国国有银行信用风险管理的启示

多年来信用风险都是各国银行所面临的主要风险,由于历史的原因我国国有银行的信用风险管理问题显得更为突出.针对国有银行信用风险管理现状,引入最新的金融工程的方法和理念,从技术创新和制度创新的角度对国有银行的信用风险管理提出建议.     

GPS based onboard and onground orbit operations for small satellites

In extension to common applications such as groundtrack displays and antenna steering, the SGP4 orbit model is proposed for operational orbit determination in small satellite missions. SGP4 is an analytical orbit model for Low-Earth orbiting satellites that is widely used for the propagation of NORAD twoline elements. Twoline elements may hence be generated completely independent of NORAD. Their use as exclusive source of orbital information simplifies the operations concept and reduces mission costs through the extensive use of existing low-cost mission support software. Due to small computer resource requirements of 8–10kByte, the SGP4 model may also be applied for onboard orbit computations making use of e.g. a 80186 processor, thus ensuring full compatibility of ground-based and onboard operations. The proposed approach is particularly suited in combination with a space-borne GPS receiver, were the C/A-code navigation solutions are treated as measurements that are adjusted in a least-squares sense using the SGP4 model. As consequence, inherent drawbacks of the pure navigation solutions such as data gaps and scatter as well as limited velocity accuracy are avoided, while the operational navigation activities are kept at a minimum. The feasibility of the concept is illustrated based on real GPS navigation data from the TOPEX/Poseidon and the MIR space station with an inherent data quality of 50–100 m. It is shown that 3 hours of data within a 4 day period are sufficient to keep the position error within 4 km, that is considered sufficient for most applications.     

k-ε-g紊流燃烧模型数值研究

本文对k-ε-g紊流燃烧模型中模型系数C_R,C_(g1),C_(g2)的选定和计算浓度脉动均方值g的不同方法进行数值研究。计算结果表明模型系数值的选定直接与化学反应速率有关,而其中C_R影响最大。g的计算虽然可有不同方法,而其中微分方程求解最佳。并用实验数据来验证计算结果。     

MTS协调加载系统建立试验载荷谱软件的设计和应用

针对MTS协调加载系统在建立试验载荷谱中存在的功能缺陷，采用多线程和动态建立索引的方法，开发了MTS协调加载系统快速、准确地建立试验载荷谱软件。介绍了软件的设计思路以及建立载荷数据模块及配置载荷情况模块及加载顺序模块等功能模块和接口的设计。解决了该系统在实际应用中存在的局限性问题，完善了MTS系统功能。最后通过试验验证了软件的实用性。     

低空突防任务下综合飞行/推进系统的建模与仿真

建立了综合飞行／推进系统的数学模型，介绍了飞机全维非线性数学模型和涡轮风扇发动机非线性部件级数学模型的建模及综合方法。对飞机执行地形中随任务时，飞行员调节飞行速度的方法与基于总能量的调节飞行速度的方法进行了比较。结果表明，基于总能量的方法比飞行员直接控制飞行速度能够减小发动机的燃油消耗，降低发动机的磨损，进而可以增加飞机的航程，延长发动机的使用寿命。     

三角面元灰度图象三维重建算法研究

三角面元SFS算法是结合三角面元模型和线性反射图来阐述SFS问题的,该算法的基本思想是用三角面元素来近似光滑表面,并用一系列基于节点的线性方程组合来表达该表面。本文在此算法的基础上,求解时通过加权平均迭代,提高了恢复的准确性和迭代的收敛速度。     

尾支杆干扰非线性修正方法的初步研究

利用CFD方法 ,采用两套网格重叠的形式 ,研究了一种对尾支杆干扰进行修正的非线性方法。运用本方法 ,研究了尾支杆等直段长度、直径和锥角对模型气动特性的影响 ,研究了四个模型有攻角时的尾支杆干扰 ,并对GBM 0 4A模型的零阻进行了尾支杆干扰的修正。     

热泵技术在旅游船废热回收上的应用研究

旅游船上的废热水以往都是通过直接排放的方式排入周围的环境中,造成较大的热污染和能源浪费;分析了热泵系统余热利用的工艺特点。利用热泵技术可以较好地回收这部分余热,降低生产的能耗。实验研究和现场应用表明利用热泵回收余热水具有比较大的节能潜力和广阔的应用前景。