Fault mode probability factor based fault-tolerant control for dissimilar redundant actuation system

This paper presents a Fault Mode Probability Factor (FMPF) based Fault-Tolerant Control (FTC) strategy for multiple faults of Dissimilar Redundant Actuation System (DRAS) composed of Hydraulic Actuator (HA) and Electro-Hydrostatic Actuator (EHA). The long-term service and severe working conditions can result in multiple gradual faults which can ultimately degrade the system performance, resulting in the system model drift into the fault state characterized with parameter uncertainty. The paper proposes to address this problem by using the historical statistics of the multiple gradual faults and the proposed FMPF to amend the system model with parameter uncertainty. To balance the system model precision and computation time, a Moving Window (MW) method is used to determine the applied historical statistics. The FMPF based FTC strategy is developed for the amended system model where the system estimation and Linear Quadratic Regulator (LQR) are updated at the end of system sampling period. The simulations of DRAS system subjected to multiple faults have been performed and the results indicate the effectiveness of the proposed approach.     

Simulation and Analysis of Electromagnetic Force in Laser Melting Deposition by Electromagnetic Impact

Magnetic field was introduced in laser melting deposition to reduce the pores in workpieces.Finite 3-D model of the coil-deposition layer-substrate was established.Simulation results show that the electromagnetic force in deposition layer mainly concentrates in the projection area of the coil.Axial electromagnetic force shows repulsion in one cycle.The experimental results indicate that the magnetic field is beneficial for grain refinement,microhardness increasement and decline of quantities and average sizes of pores.     

一种飞机大仰角飞行的模糊控制方法

提出了一种飞机大仰角飞行的动态逆模糊集成控制方法。首先使用动态逆方法求得系统的逆，使系统反馈线性化，然后，用具有在线规则自调整的模糊控制方法来确保系统的最终特性。该方法应用在高性能收音机俯仰机动指令系统的设计中，仿真结果表明，所设计的控制器满足操纵品质的要求，并且，在大仰角飞行时具有较好的鲁棒性。     

固体火箭药柱泊松比的表征与诊断

本文提出表征固体火箭药柱泊松比的三个精确表达式和一种数值积分算法。通过实验与计算给出一种固体推进剂药柱黏弹性泊松比的结果，分析了药柱黏弹性泊松比的表征与诊断以及诊断精度的有关问题。该文的结果对固体火箭发动机装药结构完整性分析计算有重要的实用价值。     

考虑辐射的化学平衡流驻点线解

本文用数值方法求解了化学平衡的高超声速粘性激波层驻点线流场。考虑了辐射和质量引射对流场的影响。辐射模型采用线和连续谱模型。文中讨论了引射率、头部半径、来流速度对壁面传热的影响。与有关文献结果比较表明,本文的方法是可行的。     

一种新型阀瓣结构

在航天器中,一般使用推力器作为姿控、轨控执行元件,推力器中的电磁阀动密封常使用和推进剂相容的橡胶材料.本文介绍一种不用过渡层硫化成型的阀瓣结构,并指出这种结构较目前流行的阀瓣结构所拥有的优越性.     

卡尔曼滤波动态优化及其在遥控机器人空间实验中应用

本文是在文献[1]的基础上,讨论遥控机器人追踪自由飞行目标物的动态性能问题。应用黄金分割法和元素交替极小化法对扩展的卡尔曼滤波初值条件进行搜索并获得优化解。仿真结果表明优化方法简单可行,优化解满足系统性能要求。     

1/spl phi/ 3W grid-connection PV power inverter with partial active power filter

This paper presents a single-phase three-wire (1/spl phi/ 3W) grid-connection photovoltaic (PV) power inverter with a of partial active power filter (PAPF) feature, which can not only deal with PV power but filter current harmonics and improve power factor. Once the processed power exceeds the switch ratings, the inverter can reduce its output reactive power and harmonic power, while still supplying the maximum real power generated by the PV arrays. In the derivation of control laws, a limit circle is defined to confine the output power of the inverter. To determine the power that the inverter can process, the instantaneous reactive power of a 1/spl phi/ 3W system is defined and used to calculate reactive power, which can avoid complex detections of phase angle and magnitude of the fundamental component of a nonlinear load current. Simulation results and experimental measurements have verified the proposed algorithm and the feasibility of the inverter.     

数据采集系统的总体评价

从性能指标出发，综述了数据采集系统总结评价技术的发展状况。并提出了对数据采集系统性能指标的两类分类方法 。     

中频比较辐射计的设计和实验

叙述了 3mm中频比较辐射计的工作原理、电路结构、特性分析及实验结果 ,研究表明 ,这种辐射计不需 3mm开关 ,其稳定性优于全功率辐射计 ,而成本和尺寸均与全功率辐射计相差不大 ,完全可以满足小型化、实用化的需要。