利用实际飞行数据插值的INS/GNSS组合导航仿真轨迹发生器

针对INS/GNSS组合导航仿真中捷联惯导系统陀螺、加速度计信号高精度模拟问题,提出基于实际飞行数据插值的动态轨迹解析生成仿真算法。对转换到地心惯性坐标系中的载体姿态、位置和重力场数据进行关于时间的样条函数插值,得到载体坐标系下陀螺角速率、角增量以及加速度计比力积分增量的高精度分段解析表达式。使生成的陀螺、加速度计信号符合载体运动学和动力学特性,反映杆臂效应影响,同时与经事后处理的实测GNSS伪距、伪距率等数据特征保持一致。提出四元数约束插值算法,其可满足四元数解析插值时范数为1的约束限制条件。基于某实际无人机飞行数据,验证了所提算法的有效性,其完全满足组合导航动态仿真精度要求。该算法也适用于其他高精度高动态导航系统和刚体运动控制仿真中的角运动、线运动传感器信号模拟。     

Complexity and workload considerations in product mix decisions under the theory of constraints

The literature on the product mix decision (or master production scheduling) under the Theory of Constraints (TOC), which was developed in the past two decades, has addressed this problem as a static operational decision. Consequently, the developed solution techniques do not consider the system's dynamism and the associated challenges arising from the complexity of operations during the implementation of master production schedules. This paper aims to address this gap by developing a new heuristic approach for master production scheduling under the TOC philosophy that considers the main operational factors that influence actual throughput after implementation of the detailed schedule. We examine the validity of the proposed heuristic by comparison to Integer Linear Programming and two heuristics in a wide range of scenarios using simulation modelling. Statistical analyses indicate that the new algorithm leads to significantly enhanced performance during implementation for problems with setup times. The findings show that the bottleneck identification approach in current methods in the TOC literature is not effective and accurate for complex operations in real‐world job shop systems. This study contributes to the literature on master production scheduling and product mix decisions by enhancing the likelihood of achieving anticipated throughput during the implementation of the detailed schedule. © 2015 Wiley Periodicals, Inc. Naval Research Logistics 62: 357–369, 2015     

GNSS/INS超紧组合导航综述

卫星/惯性超紧组合导航系统以其定位精度高、动态性能优良、抗干扰能力强等特性成为组合导航领域的研究热点。介绍了卫星/惯性超紧组合的定位原理,基于对技术原理的分析,比较超紧组合模式相对于其他组合模式的优势特点;以高动态下超紧组合技术及卫星/微惯性单元超紧组合为代表介绍国内外研究现状;总结了亟待研究的容错控制技术、神经网络辅助、多传感器辅助超紧组合等关键技术,并对卫星/惯性超紧组合向着低成本、高精度、强稳定趋势发展的前景进行展望。     

艺坛大师 教育楷模——徐悲鸿其人其事论略

徐悲鸿先生是我国著名的绘画艺术大师,艺术教育的先驱和楷模。重温他的生平事迹、艺术历程以及他那热爱祖国、献身教育、礼贤下士、为人师表的高尚品德,对当代大学生的爱国主义精神和思想品德教育具有现实意义。     

Predicting intensive care unit bed occupancy for integrated operating room scheduling via neural networks

In a master surgery scheduling (MSS) problem, a hospital's operating room (OR) capacity is assigned to different medical specialties. This task is critical since the risk of assigning too much or too little OR time to a specialty is associated with overtime or deficit hours of the staff, deferral or delay of surgeries, and unsatisfied—or even endangered—patients. Most MSS approaches in the literature focus only on the OR while neglecting the impact on downstream units or reflect a simplified version of the real‐world situation. We present the first prediction model for the integrated OR scheduling problem based on machine learning. Our three‐step approach focuses on the intensive care unit (ICU) and reflects elective and urgent patients, inpatients and outpatients, and all possible paths through the hospital. We provide an empirical evaluation of our method with surgery data for Universitätsklinikum Augsburg, a German tertiary care hospital with 1700 beds. We show that our model outperforms a state‐of‐the‐art model by 43% in number of predicted beds. Our model can be used as supporting tool for hospital managers or incorporated in an optimization model. Eventually, we provide guidance to support hospital managers in scheduling surgeries more efficiently.     

舰载火力与指挥控制系统中数字通信接口软件的可靠性设计

介绍了一种基于ＲＳ－４２２Ａ的接口软件设计,讨论了它的工作原理及在目标样机上软件可靠性设计的实现过程,建立了一种适用于主从关系的通信模式。     

GPS姿态测量系统对惯性导航系统误差修正能力分析

针对惯性导航系统(INS)存在积累误差的缺陷,运用GPS姿态测量辅助修正方法对INS误差进行补偿来进一步提高INS的定位精度.通过对INS系统可观测性进行分析,得出增加不同种类的外部导航信息观测量将有效提高INS误差修正能力的结论.研究了船用INS与GPS姿态测量系统组合的组合导航系统,并对GPS姿态测量系统信息对惯性导航系统的误差修正能力进行了仿真.仿真结果证实上述方法可有效提高INS的定位精度.     

基于事务级模型的火控计算机建模研究

在对系统进行高层次建模和验证时,事务级模型得到越来越广泛的应用。在SystemC语言的基础上构建了火控计算机的事务级模型,并通过事务级的仿真,对模型的功能进行了验证,为下一步的软硬划分和硬件设计打好基础。     

基于实际飞行数据插值的INS/GNSS组合导航仿真轨迹发生器

针对INS/GNSS组合导航仿真中,捷联惯导系统陀螺、加速度计信号高精度模拟问题,提出了基于实际飞行数据插值的动态轨迹解析生成仿真算法。对转换到地心惯性坐标系中的载体姿态、位置和重力场数据进行关于时间的样条函数插值,得到载体坐标系下陀螺角速率、角增量以及加速度计比力积分增量的高精度分段解析表达式。使生成的陀螺、加速度计信号符合载体运动学和动力学特性,反映杆臂效应影响,同时与经事后处理的实测GNSS伪距、伪距率等数据特征保持一致。提出了四元数约束插值算法,可满足四元数解析插值时范数为1的约束限制条件。基于某实际无人机飞行数据,验证了所提出算法的有效性,完全满足组合导航动态仿真精度要求。该算法也适用于其他高精度高动态导航系统和刚体运动控制仿真中的角运动、线运动传感器信号模拟。     

基于自适应滤波的GPS/INS数据融合算法

研究了高动态环境下的GPS/INS组合导航系统,重点讨论了基于伪距、伪距率的GPS/INS数据融合算法.借助于载体的运动模型、GPS系统和INS系统的定位误差模型,建立了组合导航系统的状态方程和量测方程,利用自适应Kalman滤波算法实现了GPS/INS系统的伪距、伪距率融合.最后,利用实测数据对数据融合算法进行了仿真,结果显示该数据融合算法能够增强组合导航系统的精度、可靠性和完备性.