Parallel operation of shunt active power filters with capacitylimitation control

This paper presents a capacity-limitation technique to enlarge the power capacity that can be handled by the shunt active power filters (APFs). The capacity limited includes the reactive power as well as the amplitude of the distortion current supplied by the APFs. Under capacity-limitation control m+1 APFs supply the load reactive power with m APFs supplying their rated power and one APF supplying a fraction of its rated value. Similarly, n+1 APFs supply the load current harmonic with n APFs supplying the distortion current limited in amplitude and one APF supplying a fraction of its limited amplitude. Advantages of the proposed approach include high flexibility for extending system capacity, high reliability due to no control interconnection, reducing power capacity demand of APF, high modularity due to identical APFs, stable reactive power and harmonic current sharing and its performance is insensitive to parameters mismatch of APFs, cost-effective due to modularization, and so on. Three single-phase 1 KVA APFs are designed and implemented. The effectiveness is demonstrated by some experimental results     

Reconfiguration of flight control systems for actuator failures

We consider the problem of designing fault tolerant control for transient failures in the flight control system caused by harsh electromagnetic environments. We examine principles of fault tolerant design and discuss integrated local supervisory control of these systems. As an example, we present a sample design of a control mixer to achieve fault tolerance in the event of failures in the actuators     

Neal-Smith 准则和ωspTθ2,ζsp,τθ准则的比较

军用标准1797A(MIL-STD-1797A)提供了6种不同的方法评估短周期俯仰响应。这6种方法的评价结果不完全一致。运用序列二次规划方法把ωspTθ2，ζsp，τθ准则映射到Neal—Smith准则中．以确定它们的一致区域和矛盾区域，然后改变ωspTθ2，ζsp，τθ准则中的某个参数进行分析．评估其变化趋势。     

Performance evaluation of multi-sensor classification systems

A common problem in classification is to use one/more sensors to observe repeated measurements of a target's features/attributes, and in turn update the targets' posterior classification probabilities to aid in target identification. This paper addresses the following questions: 1. How do we quantify the classification performance of a sensor? 2. What happens to the posterior probabilities as the number of measurements increase? 3. Will the targets be classified correctly? While the Kalman filter allows for off-line estimation of kinematic performance (covariance matrix), a comparable approach for studying classification accuracy has not been done previously. We develop a new analytical approach for computing the long-run classification performance of a sensor and also present recursive formulas for efficient calculation of the same. We show that, under a minimal condition, a sensor will eventually classify all targets perfectly. We also develop a methodology for evaluating the classification performance of multi-sensor fusion systems involving sensors of varying quality. The contributions of this paper are 1. A simple metric to quantify a sensor's ability to discriminate between the targets being identified, and its use in comparing multiple sensors, 2. An approximate formula based on this metric to compute off-line estimates of the rate of convergence toward perfect classification, and the number of measurements required to achieve a desired level of classification accuracy, and 3. The use of this metric to evaluate classification performance of multi-sensor fusion systems.     

表面粗糙度对航空液压作动器密封性能的影响

航空液压作动器普遍应用在飞机机翼、舱门、起落架等部位,往复密封为其典型密封形式,密封失效会 严重影响飞机任务的执行和飞行安全。密封副表面粗糙度是重要的工程可控参数且对于密封性能的影响很 大,因此分析表面粗糙度对作动器密封性能的影响具有重要的理论和实际意义。建立适用于往复组合密封的 确定性混合润滑数值仿真模型,并与有限元分析方法结合计算膜厚值,分析密封圈表面粗糙的幅值和波长变化 以及运动速度和液压油黏度变化对密封圈润滑性能和密封性能的影响。结果表明:正弦粗糙表面的幅值和波 长增大,会引起油膜压力和油膜厚度波动的幅值增大,但会减小摩擦系数;正弦粗糙表面的幅值增大,有利于减 小密封间隙的最小膜厚和泄漏量,但是波长变化的影响作用不大;液压油黏度和活塞运动速度增大,有利于增 大密封间隙油膜厚度,但会增大泄漏量和摩擦系数。     

某型飞机机载设备寿命控制方法

某型飞机的机载设备数量庞大以及寿命的不统一给维修保障工作带来了极大的不便。在研究航空机载设备的定延寿的途径和方法的基础上,分析寿命控制过程。实例显示能够简化维修保障工作,节约经费开支。     

《企业员工工作绩效问卷》的编制

绩效评估是测量和开发组织中个人的绩效的过程。它是一种重要的管理工具,与计划、组织、指挥和控制等四种主要管理职能有关,是组织决定奖惩、晋升、培训及解雇的重要依据,更是人事选拔效度研究中的效标,因而一直备受心理学家的关注。本文在文献分析与开放式问卷的基础上,编制了《企业员工工作绩效问卷》,通过对问卷探索性因素分析后,形成正式问卷。分析表明,该量表具有较好的信度和效度。     

Methodology for Multiaircraft Minimum Noise Impact Landing Trajectories

The problem of optimizing landing trajectories with respect to noise impact index is addressed. In contrast with previous work, multilandings are considered. In order to make the problem tractable the trajectories are specified in functional form with certain parameters left free for selection by the optimization methods. Constraint of aircraft dynamic behavior, trajectory separation, pilot workload, passenger comfort, and maximum noise intensity all enter into the determination of what is an allowable trajectory. A version of the quasi-Newton iterative procedure is used to determine the optimum parameter values. The results show improvement in noise impact to the airport considered and the potential for even greater improvement at many airports.     

Power Inversion Array in a Rotating Source Environment

The steady state performance of the Frost power inversion array is evaluated, assuming constant rotational velocity of the external noise environment in the sin ? domain. The weight vector is solved implicitly in terms of a linear matrix equation. Approximate criteria are derived for weight vector and output power deviation from optimal values, which are then applied to determine the maximum scan rate of a radar sidelobe canceler.     

SMESE (SMall Explorer for Solar Eruptions): A microsatellite mission with combined solar payload

The SMESE (SMall Explorer for Solar Eruptions) mission is a microsatellite proposed by France and China. The payload of SMESE consists of three packages: LYOT (a Lyman α imager and a Lyman α coronagraph), DESIR (an Infra-red Telescope working at 35–80 and 100–250 μm), and HEBS (a High Energy Burst Spectrometer working in X- and gamma-rays).