设备性能参数库两种概念模型的设计与分析

从分析电子战设备性能参数的数据特点入手,总结了设备性能参数库实体关系模式和竖表模式两种概念模型的设计思路、关键技术及其优缺点和适用性。工程应用结果表明,实体关系模式适用于从属仿真系统的数据库子系统;竖表模式适用于独立的情报数据库系统。     

质谱薄膜联用小型气体泄漏检测仪研制

传统的监测技术在往往采用单一的方法或者采用质谱加色谱联用的技术，设备大都比较笨重，操作复杂，随着现代工业的发展，急需研制体积小，质量轻在便携式仪器，同时具备灵敏度高，分辨能力强，可靠性高等特点的检测仪。利用质谱检测的高分辨能力和敏感膜的高灵敏度，文章提出了质谱和加薄膜联用进行气体泄漏监测的全新思路，并主要论述了检测仪的研制和性能实验研究等内容，最后结合其在航天领域的应用，对甲基膨，无水肼等气体进行     

飞机钣金零件弯边自动展开系统

由于飞机钣金件的复杂性,普通钣金展开软件不适合该类弯边零件的展开.本文分析了飞机钣金零件独有的特征,研究开发了基于CATIA环境下的飞机钣金零件的弯边自动展开系统,提出了一套特有的法向截面展开方法和下陷处理方法,并以实例说明零件的展开过程.     

运载火箭发射场无人值守加注发射技术研究

针对我国火箭在发射场射前操作项目多、保障人员多的问题，分析了国内外火箭发射场无人值守加注发射的现状。结合火箭射前状态，从火箭系统、地面测发控系统和发射场系统等方面提出了无人值守加注发射总体方案，通过火箭状态远程监测及故障处理技术、连接器零秒脱落技术、箭地接口组合连接技术、连接器自动对接技术和火工品自动短路保护与解保技术等关键技术研究，可提高人员和产品的安全性，为后续我国火箭实现无人值守加注发射提供参考。     

Initial virtual flight test for a dynamically similar aircraft model with control augmentation system

To satisfy the validation requirements of flight control law for advanced aircraft,a wind tunnel based virtual flight testing has been implemented in a low speed wind tunnel.A 3-degree-offreedom gimbal,ventrally installed in the model,was used in conjunction with an actively controlled dynamically similar model of aircraft,which was equipped with the inertial measurement unit,attitude and heading reference system,embedded computer and servo-actuators.The model,which could be rotated around its center of gravity freely by the aerodynamic moments,together with the flow field,operator and real time control system made up the closed-loop testing circuit.The model is statically unstable in longitudinal direction,and it can fly stably in wind tunnel with the function of control augmentation of the flight control laws.The experimental results indicate that the model responds well to the operator's instructions.The response of the model in the tests shows reasonable agreement with the simulation results.The difference of response of angle of attack is less than 0.5°.The effect of stability augmentation and attitude control law was validated in the test,meanwhile the feasibility of virtual flight test technique treated as preliminary evaluation tool for advanced flight vehicle configuration research was also verified.     

KJY-Ⅱ型精密孔径仪研制中的质量管理

科研成果商品化是我们科研所走向市场的途径之一，而商品化最重要的环节是生产过程的质量管理。本文介绍了在KJY-Ⅱ型精密孔径仪研制中取得的质量管理经验，其中一些内容涉及了小批量生产的质量管理规律。     

微型厢式货车前围外盖板引伸模加工

前围外盖板是微型厢式货车上的一个重要大型覆盖件,制件成形和模具制造难度较大,本文重点介绍该件引伸模制造过程中所采用的工艺方法.     

单框架控制力矩陀螺复合操纵律设计

为改善单框架控制力矩陀螺(SGCMG)动态操纵律的奇异回避和逃逸性能,文章设计了一种基于前馈和反馈的复合操纵律.当SGCMG系统远离奇异时,不引入前馈,仅采用基于反馈的动态操纵律;当SGCMG系统接近或陷入奇异时,在动态操纵律的基础上,引入前馈信息,辅助SGCMG系统回避或逃逸奇异.复合操纵律不但可以保留动态操纵律的优点,不需计算Jacobi矩阵的伪逆,计算简单,易于实现,而且可以逃逸椭圆型内部奇点.对某SGCMG系统的仿真结果表明,复合操纵律是可行的.     

A 3D hybrid grid generation technique and a multigrid/parallel algorithm based on anisotropic agglomeration approach

A hybrid grid generation technique and a multigrid/parallel algorithm are presented in this paper for turbulence flow simulations over three-dimensional (3D) complex geometries. The hybrid grid generation technique is based on an agglomeration method of anisotropic tetrahedrons. Firstly, the complex computational domain is covered by pure tetrahedral grids, in which anisotropic tetrahedrons are adopted to discrete the boundary layer and isotropic tetrahedrons in the outer field. Then, the anisotropic tetrahedrons in the boundary layer are agglomerated to generate prismatic grids. The agglomeration method can improve the grid quality in boundary layer and reduce the grid quantity to enhance the numerical accuracy and efficiency. In order to accelerate the convergence history, a multigrid/parallel algorithm is developed also based on anisotropic agglomeration approach. The numerical results demonstrate the excellent accelerating capability of this multigrid method.     

人机闭环组合特性试验研究

综合介绍ＢＷ－１变稳飞机测定人机闭环组合特性的试验方法，驾驶员评定方法及试验数据的分析内容。在ＢＷ－１变稳飞机试验中，用驾驶员的定性分析数据与仪器记录的定量分析数据结合起来综合权衡的方法测定人机闭环组合特性。