国外老龄化飞机结构健康监控方法

由于经济原因,国外多国军方都不得不通过延长现役飞机的寿命来维持老龄化飞机的使用。老龄化飞机在机身、蒙皮、支撑件、起落架和装配托架等位置可能出现金属疲劳裂纹,而且腐蚀影响也会使材料性能降低至失效临界点。本文旨在讨论通过有效的结构健康监控手段与方法,实现基于状态的维修,基于此提出的综合变化检测方法将有助于飞机寿命的延长。     

飞机轮胎自动充气与检测装置的研制

为了减轻飞机轮胎的充气与检测工作量，提高工作效率，增加操作时的安全性．研制了一种飞机轮胎自动充气与检测装置。试验结果表明，该装置性能可靠、工作安全、使用范围宽、使用效率高，具有国内领先水平。     

波音737NG飞机发动机过热/火警探测系统故障放行分析

介绍了波音737NG系列飞机发动机过热/火警探测系统的工作原理,针对处理探测器信号的判断逻辑和系统设计特点,给出了对发动机过热/火警系统故障放行的一些看法。     

Model-based robust estimation and fault detection for MEMS-INS/GPS integrated navigation systems

In micro-electro-mechanical system based inertial navigation system（MEMS-INS）/global position system（GPS） integrated navigation systems, there exist unknown disturbances and abnormal measurements. In order to obtain high estimation accuracy and enhance detection sensitivity to faults in measurements, this paper deals with the problem of model-based robust estimation（RE） and fault detection（FD）. A filter gain matrix and a post-filter are designed to obtain a RE and FD algorithm with current measurements, which is different from most of the existing priori filters using measurements in one-step delay. With the designed filter gain matrix, the H-infinity norm of the transfer function from noise inputs to estimation error outputs is limited within a certain range; with the designed post-filter, the residual signal is robust to disturbances but sensitive to faults. Therefore, the algorithm can guarantee small estimation errors in the presence of disturbances and have high sensitivity to faults. The proposed method is evaluated in an integrated navigation system, and the simulation results show that it is more effective in position estimation and fault signal detection than priori RE and FD algorithms.     

基于直线成像特征的视觉测量系统综合标定方法

针对视觉测量系统存在复杂系统误差的特点,提出一种基于直线成像特征的系统综合标定方法,有效地保证了测量精度.该方法通过对1等量块的平行直线边缘提取,建立量块边缘空间物点位置和像点位置的原始对应关系,利用量块边缘的理想直线特征,通过统计计算对测量系统进行综合标定,建立描述空间物点位置和像点位置的相互对应关系的二元三次标定函数.对在测量范围内不同方位的量块进行多次测量,表明使用这种标定方法标定的视觉测量系统的测量精度能够达到.     

基于自适应模糊逻辑的活塞发动机TCU故障检测算法研究

故障分析与诊断是活塞发动机地面试车检测系统的关键功能之一,对于确保试飞安全具有重大意义。通过分析模糊逻辑系统的数学原理,研究了基于模糊逻辑的故障诊断模块分析算法,并利用MALLAB软件实现了模块基本功能,为利用模糊逻辑算法的非线性逼近能力,分析并监测发动机TCU运行状态奠定了基础。     

接收机自主完好性监测技术研究

对卫星接收机完好性监测技术进行了简单的介绍,以最小二乘法对接收机自主完好性监测(Receiver Autonomous Integrity Monitoring,RAIM)的基本公式进行了详细的推导和分析,以奇偶矢量法在实际工程应用中验证了RAIM算法的正确性和可行性。在此基础上,提出一种新的故障卫星排除算法－均方根（Root Mean Square,RMS）比较法,工程验证了算法的有效性,具有较强工程应用价值。     

具有分时段智能运行的节能扶梯改造方案

针对当前商场扶梯的固有缺点,介绍一种具有分时段智能运行,具有较大节能潜力的商场扶梯变频改造方案,实现节能降耗、延长扶梯使用寿命的目的.     

A Fault-tolerance Estimating Method for Ionosphere Corrections in Satellite Navigation System

 Aiming to the reliable estimates of the ionosphere differential corrections for the satellite navigation system in the presence of the ionosphere anomaly, a fault-tolerance estimating method, which is based on the distributed Kalman filtering, is proposed. The method utilizes the parallel sub-filters for estimating the ionosphere differential corrections. Meanwhile, an infinite norm (IN) method is proposed for the detection of the ionosphere irregularity in the filter processing. Once the anomaly is detected, the sub-filter contaminated by the anomaly measurements will be excluded to ensure the reliability of the estimates. The simulation is conducted to validate the method and the results indicate that the anomaly can be found timely due to the novel fault detection method based on the infinite norm. Because of the parallel sub-filter architecture, the measurements are classified by the spatial distribution so that the ionosphere anomaly can be positioned and excluded more easily. Thus, the method can provide the robust and accurate ionosphere differential corrections.