大型空间运动体的建模

本文建立了大型空间运动体的模态方程,并利用模态方程导出传递函数矩阵,给出离散传递函数矩阵的分解形式。利用这种方法对控制系统进行设计和频域分析。     

基于CPLD的IRIG-B码源的实现

介绍一种基于 CPL D的 IRIG- B码码源的设计思想和实现方法 ,并给出实验结果。所产生的标准串行时间码可用于测量设备 ,解决测量设备在时间上的统一问题 ;也可作为实践教学设备使用 ,让学员了解 IRIG- B码的结构及工作流程。采用可编程逻辑器件来实现 ,使系统小型化、集成度高、可编程性好 ,适应未来微电子技术的发展要求。     

A novel unified model predicting flow stress and grain size evolutions during hot working of non-uniform as-cast 42CrMo billets

The cast preformed forming process(CPFP) is increasingly considered and applied in the metal forming industries due to its short process, low cost, and environmental friendliness, especially in the aerospace field. However, how to establish a unified model of a non-uniform as-cast billet depicting the flow stress and microstructure evolution behaviors during hot working is the key to microstructure prediction and parameter optimization of the CPFP. In this work, hot compression tests are performed using a non-uniform as-cast 42 CrMo billet at 1123–1423 K and 0.01–1sà1. The effect laws of the non-uniform state of the as-cast billet with different initial grain sizes on the flow stress and microstructure are revealed deeply. Based on experimental results, a unified model of flow stress and grain size evolutions is developed by the internal variable modeling method. Verified results show that the model can well describe the responses of the flow stress and microstructure to deformation conditions and initial grain sizes. To further evaluate its reliability, the unified model is applied to FE simulation of the cast preformed ring rolling process.The predictions of the rolling force and grain size indicate that it could well describe the flow stress and microstructure evolutions during the process.     

多航天器交会下天地通信工作模式探讨

针对中国空间站工程航天器交会对接任务中,地面与多航天器同时进行天地话音和图像通信的潜在需求,分析TDRSS（TrackingandDataRelaySatelliteSystem,跟踪与数据中继卫星系统）、USB（UnifiedSBand,统一S频段）测控通信系统及天地通信中心系统支持多目标同时通信的技术原理,提出天地通信系统在双目标、三目标同时跟踪时的工作模式,介绍天地通信系统仿真验证体系,并重点阐述天地通信中心如何采用环回和回放数据文件的仿真方法验证系统对多目标的支持,由此表明天地通信系统具备同时与多航天器进行通信的能力。探讨的结果对工程和实际应用具有参考和借鉴价值。     

基于UML自动化立体仓库管理系统的建模方法

本文结合实例讨论了运用UML的机制为复杂系统建模的方法。建立了自动化立体仓库管理系统的分析模型，并给出部分用倒图、类图以及交互图。简述UML技术与软件复用的关系。     

Asymmetric magnetic field inside a cylindrical flux rope

In order to consider an asymmetric field distribution inside a cylindrical tube with a circular cross section, with the field magnitude maximum reached at a point different from the geometrical centre of the tube, we propose a new solution obtained in bi-cylindrical coordinates. If the parameter of the system is very large, the solution approaches the well known symmetric Lundquist solution. The new solution models a field magnitude shift due to relative motion of the cylinder and the ambient solar wind. If the cylinder is moving much faster than the ambient medium, its field maximum is shifted forward, otherwise it is shifted in the opposite direction.     

Short-term forecasting regional model to predict M(3000)F2 over the European sector: Comparisons with the IRI model during moderate,disturbed, and very disturbed geomagnetic conditions

The hourly measurements of M(3000)F2 (M(3000)F2_meas) and the hourly quiet-time values of M(3000)F2 (M(3000)F2_QT) relative to the ionospheric observatories of Poitiers, Lannion, Dourbes, Slough, Rome, Juliusruh, Kaliningrad, Uppsala, Lyckesele, Sodankyla, and Kiruna as well as the hourly time-weighted accumulation series derived from the geomagnetic planetary index ap (ap(τ)), were considered during the period January 1957–December 2003 and used for the development of 11 short-term forecasting local models (STFLM) of M(3000)F2.     

大学英语课堂环境的优化与改善

针对大学大班英语课堂教学出现的问题,教师应以二语习得理论为指导,通过创造课堂全外语教学沉浸式的自然习得环境,采取灵活多样的教学方法和授课方式,组织互动式的课堂活动,并且在教学中注意加强情感教学,降低学生学习焦虑感,从而优化大班英语课堂教学环境,营造宽松和谐的课堂氛围。     

On the stability of flexible aircraft

The problem of aircraft stability has been a subject of concern since the beginnings of flight. Traditionally, aircraft stability has been treated within the confines of two separate disciplines, namely, flight dynamics and aeroelasticity. Based on some recent developments in the dynamics and control of flexible aircraft, this investigation uses the system concept to provide a broader approach to aircraft stability in an attempt to bridge the gap between stability as understood in flight dynamics and stability as envisioned in aeroelasticity. To this end, stability is studied in the following four cases: 1) dynamics of whole flexible aircraft using the unified formulation, 2) flight dynamics of quasi-rigid aircraft (aircraft treated as rigid), 3) aeroelasticity of flexible components, such as cantilever wing, cantilever horizontal stabilizer, etc., and 4) aeroelasticity of restrained flexible aircraft (aircraft fixed to a point, hence, having no rigid body degrees of freedom). The paper also presents a method to address the stability of flexible aircraft when the compressibility correction factor is known only at some discrete Mach numbers.     

实施统一编号 加强仪器管理

电子仪器管理的规范化是保证周期检定正常运行、量值传递准确可靠、为产品质量提供计量保证的重要方面。本文介绍了电子仪器从验收合格－建帐－使用一周检过程的管理。此方法实施六年来运行良好。