依法治国和以德治国相结合是构建和谐社会的必然选择

“依法治国”与“以德治国”是辨证地联系在一起的。对一个国家的治理来说，法治与德治从来都是相辅相成、相互促进的。尤其是要构建和谐社会，更是二者缺一不可的。     

美军主要战术数据链介绍

介绍了美国目前使用中的三种战术数据链Link 4A、Link 11和Link 16的背景,功能、特点和装备情况,同时通过列表对照了三种战术数据链技术体制的相同点和不同点。最后阐述了三种战术数据链的互操作性问题。     

Rectangle expansion A*pathfinding for grid maps

Search speed, quality of resulting paths and the cost of pre-processing are the principle evaluation metrics of a pathfinding algorithm. In this paper, a new algorithm for grid-based maps, rectangle expansion A* (REA*), is presented that improves the performance of A* significantly. REA*explores maps in units of unblocked rectangles. All unnecessary points inside the rectangles are pruned and boundaries of the rectangles (instead of individual points within those boundaries) are used as search nodes. This makes the algorithm plot fewer points and have a much shorter open list than A*. REA*returns jump and grid-optimal path points, but since the line of sight between jump points is protected by the unblocked rectangles, the resulting path of REA*is usually better than grid-optimal. The algorithm is entirely online and requires no offline pre-processing. Experi-mental results for typical benchmark problem sets show that REA*can speed up a highly optimized A* by an order of magnitude and more while preserving completeness and optimality. This new algorithm is competitive with other highly successful variants of A*.     

A320短舱/吊挂维修性设计缺陷分析

发动机短舱/吊挂的维修性设计直接影响地面维修人员对飞机的维修质量。通过对国内典型飞机发动机组合的短舱/吊挂区域维修性问题的研究,总结了A320飞机运营过程中在短舱/吊挂区域出现的问题及处理措施,为我国大型客机吊挂区域的维修性设计提供技术参考和建议。     

A320飞机起动活门故障分析

飞机发动机引气驱动起动机,起动活门的可靠性直接影响起动效率。本文对A320飞机起动活门进行分析,并提出维护建议。     

旋翼干扰下的直升机尾桨气动噪声计算研究

针对旋翼干扰下的直升机尾桨气动噪声计算问题,将CFD方法与Farassat 1A(F1A)公式相结合,提出了一种适用于旋翼干扰下的尾桨气动噪声数值计算方法。首先,应用所提出的方法进行了噪声的算例验证,并与参考文献结果进行了对比;然后,着重针对悬停和前飞状态旋翼干扰下的尾桨噪声及气动特性进行了计算分析,并与孤立尾桨状态进行了对比。计算分析结果表明:悬停状态下,旋翼干扰下的尾桨气动噪声水平显著大于孤立尾桨;而在前飞状态,由于旋翼尾迹对尾桨桨盘平面产生更强的气动干扰,这一现象会更加明显;同时,在旋翼干扰作用下,尾桨噪声的主传播方向也会发生明显变化。     

气象雷达综合测试系统的设计与实现

以某系列雷达为研究对象,详细介绍了基于PXI总线雷达综合测试系统的硬件组成和软件设计方法,并详细阐述了组建雷达综合测试系统过程中重点、难点的实现方法。实际应用表明：该系统具有通用性强、扩充性好、可靠性高等特点。     

Random copolymer membrane coated PBO fibers with significantly improved interfacial adhesion for PBO fibers/cyanate ester composites

Poly(p-phenylene-2,6-benzobisoxazole) (PBO) fibers possess excellent dielectric, mechanical properties and heat resistance. However, the surface of PBO fibers is smooth and highly chemical inert, resulting in poor interfacial compatibility to polymer matrix, which severely limits its wider application in high-performance fiber-reinforced resin matrix composites. In this work, random copolymers (P(S-co-BCB-co-MMA)) containing benzocyclobutene in the side-chain were synthesized by reversible addition-fragmentation chain transfer (RAFT) polymerization, which were then utilized to form dense random copolymer membrane on the surface of PBO fibers by thermally cross-linking at 250 °C (PBO@P fibers). Four kinds of synthesized P(S-co-BCB-co-MMA) with different number-average molar mass (M_n) were well controlled and possessed narrow dispersity. When the M_n was 32300, the surface roughness of PBO@P fibers was increased from 11 nm (PBO fibers) to 39 nm. In addition, PBO@P fibers presented the optimal interfacial compatibility with bisphenol A cyanate (BADCy) resins. And the single fiber pull-out strength of PBO@P fibers/BADCy micro-composites was 4.5 MPa, increasing by 45.2% in comparison with that of PBO fibers/BADCy micro-composites (3.1 MPa). Meantime, PBO@P fibers still retained excellent tensile strength (about 5.1 GPa). Overall, this work illustrates a simple and efficient surface functionalization method, which would provide a strong theoretical basis and technical support for controlling the surface structure & chemistry of inert substrates.     

基于A3200控制器的超精密机床控制系统的设计与应用

以一种新型的运动控制器—A3200控制器为核心搭建了数控系统硬件平台,对控制器的控制函数及直接命令进行了研究,基于机床的需求开发了数控系统软件平台。同时,结合A3200控制器与伺服系统参数整定与优化方法,对伺服系统参数进行了整定和优化,提高了系统的精确性和稳定性。最后,对半球谐振子进行了加工试验,验证了数控系统的控制性能及加工精度。     

环境减灾-1A、1B卫星供配电测试系统设计

描述了环境减灾-1A、1B卫星供配电测试系统的设计与构建方法,系统采用一套设备完成了双星的测试任务,具有集成度、可靠性高等特点。文章首先介绍了HJ-1A、1B双星供配电测试系统的硬件架构,主要包括数字量采集与控制集成化措施,基于星地隔离与卫星安全的内部功能模块设计方法,以及作为自动化测试对测试设备统筹管理的远程控制功能实现方法;其次介绍了控制与采集软件的结构与功能设计,以及软件设计过程中所采取的抗干扰措施;最后提出了供配电测试系统的设计原则,可为后续测试设备的设计提供理论与工程基础。