驱动控制对太阳帆板驱动系统动力学特性的影响

准确预示太阳帆板驱动系统动力学特性是开展扰振机理和振动控制研究的基础。本文推导了考虑驱动控制因素的太阳帆板驱动装置等效力学特性参数表达式,构建了太阳帆板驱动系统动力学特性等效分析模型,并在仿真和试验验证基础上,讨论了驱动速度和控制增益对驱动装置力学特性参数和驱动系统动力学特性的影响规律。结果表明:所构建的等效分析模型能够在不同驱动速度和控制增益情况下准确预示驱动系统动力学特性,分析结果与试验误差小于10%；驱动装置等效阻尼与驱动速度和控制增益无关,但等效刚度随控制增益减小和驱动速度增大而减弱。随着驱动速度提高,驱动控制逐渐成为影响驱动系统动力学特性的重要因素。     

飞机液压系统试验数据分析软件的研究与开发

为了解决对飞机液压系统试验数据进行全程实时观测困难这一问题,避免重复试验,以VC++为开发工具,采用面向对象的设计方法,设计了一套飞机液压系统试验数据动态回放、分析软件.并应用某型号飞机前起落架收放系统的主液压泵的工作过程试验数据对该软件进行了测试,结果表明该软件能够为飞机液压系统的试验提供有用的帮助,具有较高的应用价值.     

船艇机舱发动机辐射噪声研究

针对在混响声场发动机辐射噪声识别困难的问题,提出用统计能量分析法对船艇机舱发动机进行噪声源分析。建立了机舱发动机噪声源识别模型,计算了发动机各表面的辐射声功率大小及频率特性。应用表面振动测量法对机舱发动机各表面辐射噪声进行识别,其结果与统计能量分析法的对比表明:统计能量分析法考虑声场的反射和叠加,能更好地识别复杂声场环境下发动机辐射噪声。     

Inventory policies for a make‐to‐order system with a perishable component and fixed ordering cost

We consider a make‐to‐order production system where two major components, one nonperishable (referred to as part 1) and one perishable (part 2), are needed to fulfill a customer order. In each period, replenishment decisions for both parts need to be made jointly before demand is realized and a fixed ordering cost is incurred for the nonperishable part. We show that a simple (s_n,S,S) policy is optimal. Under this policy, S along with the number of backorders at the beginning of a period if any and the availability of the nonperishable part (part 1) determines the optimal order quantity of the perishable part (part 2), while (s_n,S) guide when and how much of part 1 to order at each state. Numerical study demonstrates that the benefits of using the joint replenishment policy can be substantial, especially when the unit costs are high and/or the profit margin is low. © 2009 Wiley Periodicals, Inc. Naval Research Logistics, 2009     

光学阵列器件的慢刀伺服车削加工技术

慢刀伺服技术是相对于快刀伺服提出的方法.采用C轴、X轴、Z轴联动的方法在极坐标或圆柱坐标内进行加工.光学阵列如微透镜阵列、微反射镜阵列在高速数据、声音和视频信号传输中具有重要作用.将光学阵列看作一个自由曲面,使用慢刀伺服车削技术一次加工成形,可以解决传统加工中将光学阵列分块加工后拼装和调整的困难.但是由于光学阵列表面形状复杂,其表面法线的突变可能会使机床运动超出伺服轴执行能力.根据慢刀伺服加工技术的特点,建立了伺服轴执行能力限制曲线,研究了不同刀具半径补偿方式对加工的影响.实验结果表明,根据机床伺服轴执,厅能力合理选择刀具半径补偿方式可实现微光学阵列器件高精度加工.     

基于模糊时间序列的时变动态系统模糊建模

要想建立结构不确定、参数时变的动态系统的模型是很困难的。改进了Song Chisson的模糊时间序列方法,并成功应用于时变动态系统的辨识与建模和自适应控制。仿真结果表明该方法计算量小,实时性好,能很快地跟踪系统的变化。     

基于高速电弧喷涂的材料制备与成形一体化技术

材料制备与成形一体化技术是装备再制造关键技术之一。对于一些难以合成及加工成形的材料,采用高速电弧喷涂粉芯丝材的方法,通过喷涂弧区的快速、动态冶金过程,同步实现新材料的合成与成形,即在再制造快速成形过程中实现新材料的合成与制备。这一技术一方面可通过新材料设计,制备出赋予零件防腐蚀、耐磨损、耐高温等性能的涂层体系,另一方面它突破了热喷涂技术只能制备薄涂层传统观念,在开展制造零件用的快速成形材料方面也具有良好的研究空间。基于高速电弧喷涂的材料制备与成形一体化技术在舰船钢结构长效防腐、电站锅炉管道防护、装备零件成形制造与再制造等领域具有良好的应用前景。     

反潜编队应召搜索能力计算及效果评估

本文在分析反潜编队应召搜索特点的基础上,对应召搜索能力进行了必要的战术计算,对应召搜索的效果进行了评估,为实际反潜作战中提高对潜搜索的效果提供了可靠的依据。     

中子增殖研究

导出了一个新的中子增殖公式,公式简明,计算量小.经与传统的增殖公式进行比较,后者由于未考虑缓发中子效应,只能用于定性分析.新导出的中子增殖公式较精确地描述了中子的增殖过程,可用于定量计算与分析.     

Integrated guidance and control of guided projectile with multiple constraints based on fuzzy adaptive and dynamic surface

Based on fuzzy adaptive and dynamic surface (FADS), an integrated guidance and control (IGC) approach was proposed for large caliber naval gun guided projectile, which was robust to target maneuver, canard dynamic characteristics, and multiple constraints, such as impact angle, limited measurement of line of sight (LOS) angle rate and nonlinear saturation of canard deflection. Initially, a strict feedback cascade model of IGC in longitudinal plane was established, and extended state observer (ESO) was designed to estimate LOS angle rate and uncertain disturbances with unknown boundary inside and outside of system, including aerodynamic parameters perturbation, target maneuver and model errors. Secondly, aiming at zeroing LOS angle tracking error and LOS angle rate in finite time, a nonsingular terminal sliding mode (NTSM) was designed with adaptive exponential reaching law. Furthermore, combining with dynamic surface, which prevented the complex differential of virtual control laws, the fuzzy adaptive systems were designed to approximate observation errors of uncertain disturbances and to reduce chatter of control law. Finally, the adaptive Nussbaum gain function was introduced to compensate nonlinear saturation of canard deflection. The LOS angle tracking error and LOS angle rate were convergent in finite time and whole system states were uniform ultimately bounded, rigorously proven by Lyapunov stability theory. Hardware-in-the-loop simulation (HILS) and digital simulation experiments both showed FADS provided guided projectile with good guidance performance while striking targets with different maneuvering forms.