抗尾流干扰的自动着舰非线性控制研究

由于飞机与尾流模型的非线性,为实现自动精确着舰,探究了具有尾流抑制能力的非线性控制器设计方法.基于气流扰动影响的飞机六自由度非线性模型,利用非线性动态逆控制方法对各控制回路进行了设计,为抑制尾流扰动,提出了应用非线性观测器进行补偿的方法.仿真结果表明,具有非线性干扰观测器的控制器可以在4s内使飞机稳定在速度为52.04 m/s,并使航迹角保持在±0.5°变化范围内,最终的着舰侧向偏差为-0.13m.     

Adaptive leader–follower formation control for swarms of unmanned aerial vehicles with motion constraints and unknown disturbances

In this paper, the 3D leader–follower formation control problem, which focuses on swarms of fixed-wing Unmanned Aerial Vehicles (UAVs) with motion constraints and disturbances, has been investigated. Original formation errors of the follower UAVs have been transformed into the Frenet-Serret frame. Formation control laws satisfying five motion constraints (i.e., linear velocity, linear acceleration, heading rate, climb rate and climb angle) have been designed. The convergence of the control laws has been discussed via the Lyapunov stability tool. In addition, to address the unknown disturbances, an adaptive disturbance observer is exploited. Furthermore, formation control laws involving estimated disturbances are presented as well. The collision avoidance between UAVs is achieved with the artificial potential method. Simulation results obtained using four scenarios verify the effectiveness of the proposed method in situations with constant disturbances and varying disturbances, as well as without disturbances.     

氦气流量校准装置的研究

简要分析了氦气流量校准装置的工作原理和结构，对系统的软、硬件及校准流程进行了讨论，提出并详细阐述了其计量容积的标定技术和计算方法，并在主标准器的结构设计上提出了新的思路，使装置的流量测量扩展不确定度可达0．03％（k=2）。     

Simultaneous spacecraft attitude and orbit estimation using magnetic field vector measurements

Based on magnetometer measurements only, three-axis attitude, rate, and orbit estimation are successfully achieved. A single Augmented Dynamics Extended Kalman Filter (ADEKF) is configured by combining the spacecraft nonlinear attitude dynamics and quaternion kinematics with orbital mechanics. The filter design is adopted for three-axis stabilized spacecraft in low Earth orbits where the aerodynamic drag is the dominant source of disturbances in addition to the spacecraft magnetic residuals. To reduce the computational burden, another Interlaced Extended Kalman Filter (IEKF) is developed to uncouple the attitude/rate from the orbit dynamics. Both filters are implemented using the magnetometer measurements and their corresponding time derivatives. As a part of EgyptSat-1 flight scenario, detumbling and standby modes are used for performance testing of the ADEKF. The concept of local observability is applied to the basic filter and the stability is investigated by incorporating extensive Monte Carlo simulations with uniformly distributed initial conditions. The filter shows the capability of estimating the attitude better than 5 deg and rate of order 0.03 deg/s in each axis. In orbit estimation, the filter is capable of estimating the position with accuracy less than 8 km and velocity upto 5 m/s in each axis.     

“嫦娥二号”卫星CCD立体相机的关键技术

文章介绍了中国两次绕月探测中 CCD 立体相机所采用的技术与创新,并与国际同类相机所获取的图像进行了比较;在此基础上详细介绍了“嫦娥二号”(CE-2)卫星CCD立体相机的综合创新集成技术--“单镜头两视角同轨立体成像、时间延迟积分图像传感器（TDICCD）推扫、速高比补偿”,并从工程目标与科学目标出发进行探测灵敏度及成像动态范围的需求分析;根据需求分析确定了总体技术方案,包括光、机、电的优化设计以及对月探测中首次采用TDICCD的技术困难与对策;特别讨论了速高比补偿的方案及实施途径,并进行了在轨试验验证。文章最后分别给出了虹湾地区成像分辨率为1.3m以及全月面分辨率为7m 的代表性图像,图像清晰、层次丰富,显示出中国在对月立体成像技术上取得了显著进步。     

开放我国资本账户面临的风险及防范

我国现阶段正依照循序渐进、统筹规划、先易后难、留有余地的原则，分阶段、有选择地逐步推出资本项目开放措施。理论研究和各国实践都证明资本账户的开放是利弊共存的，关键在于如何有效疏导和防范开放带来的系列风险，采取有力措施将资本账户开放的风险降到最低点，保证宏观经济的稳定发展。通过探讨2005年7月21日进行汇率制度改革以来，我国开放资本账户过程中所面临的银行体系风险、资本流动性过剩风险和资本流动逆转风险，提出了防范风险的对策建议。     

浅谈控制图在飞机完好率控制中的应用

为促进航空维修质量管理由事后控制向过程控制转变，应用过程控制理论的重要工具--质量控制图实现对飞机完好率的控制，结果证明该方法科学有效，可为航空维修工作的优化实施提供有力的理论指导。     

浅析提高投篮命中率的技术因素

本文分析了影响投篮命中率的各种技术因素,并提出了相应的提高命中率的方法,为篮球教学工作提供有益的参考。     

一种测量旋转条件下底排装药燃速的方法

给出了一种利用高速摄影技术测量旋转条件下底排装药燃速的方法，其测量误差小于０．８％，并建立了燃速增大系数与径向加速度之间的函数关系。从实验得出，当径向加速度达到某一临界限值时才会出现旋转效应。     

纳米铝粉热反应特性的TG-DSC研究

采用TG-DSC法对平均粒径85 nm的纳米铝粉进行了热反应特性研究,并与微米铝粉进行了对比.结果表明,铝粉热反应特性的尺度效应明显,纳米铝粉在517℃附近出现明显增重,500～660℃氧化增重20.4％,放热约4 909 J/g,而微米铝粉在600℃左右才有少量的增重,粒径越大,氧化增重越小,4～6、9～10、16～...