VxWorks下飞行模拟系统研究与设计

介绍了基于嵌入式实时操作系统VxWorks的无人机仿真系统。建立了无人机动力学及运动学数学模型,给出了气动系数的拉格朗日插值计算方法,采用一种全新的方法实现飞行模拟,即利用RTW接口下载飞机数学模型到VxWorks操作系统。最后给出了半物理仿真和全数字仿真的对比曲线,验证了仿真系统的正确性。该系统的研制成功,对于验证无人机飞控/导航控制律及加快无人机研制进度有重要意义。     

三脉冲冷原子陀螺仪中基于内态演化的拉曼光光强补偿算法

由于在复杂环境中拉曼光功率不稳定会导致原子脉冲的宽度发生改变,从而影响陀螺仪的测量精度.通过对冷原子干涉仪的干涉全过程进行建模,计算得出了陀螺仪在拉曼光改变情形下输出相位的解析表达式,即建立了拉曼光在非近共振条件下强度变化时陀螺仪的输出值与外界载体运动之间的关系.与此同时,基于该解析表达式提出了一种对拉曼光光强的补偿算...     

IPv6技术在空地通信系统中的应用

当前的空地通信方式已无法适应航空业的迅速发展。针对这一问题,本文提出建立基于甚高频数据链模式二(VDLM2)的IPv6通信系统,以将IPv6技术应用到空地通信系统中；并给出了IPv6/VDLM2通信系统的体系结构。然后,利用VDLM2的OPNET仿真模型,分析了IPv6/VDLM2通信系统的容量。分析结果表明,在给定条件下,IPv6/VDLM2通信系统可允许大约100架飞机同时与单个地面站进行通信。     

Synthesis of Iron-containing Carbon Microparticles from Deoiled Asphalt and Ferrocene

The deoiled asphalt as the carbon source and the ferrocene as the metal source and the catalyst precursor were chosen to synthe-size iron-containing carbon microparticles through co-carbonization at the temperature of about 450 ℃ for 3 h. The resulting products were treated at 2 000 ℃ for 2 h. All samples were examined by high resolution transmission electron microscopy (HRTEM) and X-ray diffraction (XRD). The results show that the iron particles in the heat-treated material are completely coated by carbon. In addition to the fully filled carbon microparticles as well as hollow carbon ones, also form carbon fibers with hollow centers. The formation mechanism of the as-prepared products was discussed briefly.     

微量元素P对NiAl-34Cr合金显微组织和力学性能的影响

采用真空非自耗电弧炉熔炼了四种P含量(0.005%,0.02%,0.05%,0.15%(质量分数))的NiAl-34Cr-xP合金.铸态合金的组织均含有NiAl相和Cr相,为典型的胞状树枝晶组织,且随着P含量的增加胞状树枝晶的平均尺寸逐渐减小.在P含量为0.05%和0.15%的合金中还存在Cr3P相.均匀化热处理后合金...     

条形碳化硅纤维的制备与性能

使用异形喷丝板通过熔融纺丝制备出条形聚碳硅烷原纤维,然后经不熔化及高温烧成得到条形碳化硅纤维。通过X射线衍射仪分析了条形碳化硅纤维的构成、强度及电磁性能。结果表明,条形碳化硅纤维主要由β-SiC和无定形SiC组成,纤维的当量直径为20~31μm,拉伸强度为0.8~2.4 GPa,介电常数实部ε′为6.2~6.8,虚部ε″为2.5~3.3。条形碳化硅纤维可用作结构吸波材料。