分布式作战指挥模拟训练系统中语音通信仿真研究*

传统的分布式作战指挥模拟训练系统中存在通信模块可控性差、操作使用复杂等问题，为此设计和实现了新型的多功能语音通信仿真系统。提出了系统的总体结构，对系统中的语音服务器、语音客户端和通话器进行了设计，详细阐述了系统涉及的四项关键技术及其实现方案。实际应用的结果表明所设计和实现的多功能语音通信仿真系统能够满足部队指挥训练的要求。     

Innovative strategies for urban car-sharing systems and a simulator to assess their performance

In this paper, three innovative car-sharing systems for urban areas are proposed, based on fleets of individual intelligent vehicles with three service characteristics: instant access, open-ended reservations and one-way trips. These features provide high flexibility but create an uneven distribution of vehicles among stations. Therefore, relocation of vehicles must be performed. Three different system procedures are proposed: in the first system, relocations are performed by users; in the other two, vehicles relocate automatically, thanks to their automation. In the first two systems, vehicles are accessible only at stations, whereas in the third they are also accessible along roads. In order to provide transport managers with a tool to test systems in different realities, an object-oriented simulator is developed. The simulation provides outputs of system performance, in terms of user waiting times and system efficiency. The proposed systems are simulated for the city of Genoa, in Italy, and a comparative analysis is presented.     

营运大客车正面碰撞乘员伤害的研究

客车发生正面碰撞事故约占客车碰撞事故的50%~60%。利用LS-DYNA软件,建立了包括假人、安全带和安全气囊在内的大客车车体有限元模型,对不同速度下营运大客车的正面碰撞特性进行了模拟仿真计算,分析了无任何保护措施、佩戴安全带及佩戴安全带且安全气囊起爆三种事故形态下乘员头部HPC值、胸部压缩量和大腿骨轴向接触力等伤害值。研究结果表明,安全带对于驾驶员的保护意义重大,为营运大客车乘员保护设计以及合理制定营运大客车正面碰撞法规提供数据参考。     

某型直流充电柜温度场仿真

对某型直流充电柜满负载工况下温度场进行仿真,根据实验测量数据验证仿真结果准确性,成功完成了对充电柜温度场的建模仿真工作,并实现对初始模型的简化,为对整个充电站进行温度场建模仿真奠定了基础。     

能量回馈型四象限电力电子负载在船舶电力系统动模试验中的应用

目前，随着船舶综合电力系统的发展，船用负载设备类型的增多导致目前交直流动模试验室无法真实模拟系统动态特性。为研究和分析能量回馈型四象限电力电子负载船舶电力系统动模试验的应用，本文通过分析四象限电力电子负载的拓扑结构和控制方式，在Matlab/Simulink仿真平台和动模试验室中分别进行了能量回馈型四象限电力电子负载相关功能试验。仿真和试验结果表明，能量回馈型四象限电力电子负载能够模拟不同类型的负载以及不同电压、功率等级的电源，并且在模拟负载时，能够将吸收的电能高效地反馈回电网，不仅可以提高工作效率，还能够起到节约电能的目的。     

喷孔位置对船用天然气发动机燃烧及排放影响的模拟研究

为了探究天然气与柴油喷孔位置对天然气发动机燃烧和排放的影响,基于L23/30天然气发动机,建立了柴油引燃天然气的发动机模型,利用CONVERGE软件对燃烧过程和排放进行模拟分析。模拟结果表明：由于天然气与柴油喷孔位置变化的影响,会导致柴油引燃天然气在空间的变化,因此对发动机的燃烧和排放造成了影响,通过对比不同喷嘴间的距离和不同喷嘴分布的设计方案得出,采用中心对称设计时获得了较好的燃烧和排放性能。     

全回转起重船多系统耦合运动响应仿真分析

根据运动学基本原理,计入船-吊物、船-锚链耦合影响以及起重船自身受到的外环境载荷,建立船舶多系统运动模型。利用MATLAB/Simulink软件进行仿真,对多系统耦合作用下的船舶运动进行数值分析。分别在不同的遭遇浪向角和不同的吊臂回转角下,对船舶在各自由度上的位移进行比较,得到其对船舶运动参数的影响规律。结果表明:起重船运动过程中因计入多系统耦合影响,自身运动也表现出更为符合实际的运动特性,为准确预报全回转起重船多系统的运动响应提供了更为科学的理论依据。     

救助船模拟器原型机关键技术研究

针对大风浪条件下救助船操纵训练的要求，有必要开发针对救助船的操纵模拟器。相比于传统的通用船舶模拟器，救助船模拟器原型机系统中引入六自由度平台运动系统，基于UDP协议传输船舶姿态数据实现实时体感模拟功能，可以模拟船舶在大风浪条件下剧烈摇动的操船环境，提高模拟训练的真实感。此外，系统中引入救助作业模拟模块的思想，可以更好地评估、训练船员在恶劣海况下配合其他救助人员完成救助任务的能力，提高执行海上救助任务的成功率与效率。     

Full six degrees of freedom coupled dynamic simulation of ship collision and grounding accidents

By taking advantage of the user-defined load subroutine (loadud) and the user common subroutine (usercomm) in LS-DYNA, the authors proposed a new coupled approach for simultaneously calculating structural damage and the planar 3DOF ship motions in ship collisions. The coupled procedure aimed at predicting the detailed structural damage together with reasonable global ship motions. This paper extends the method to consider the full 6DOF ship motions; thus, ship collision as well as grounding accidents can be properly handled. This method is particularly useful for design purposes because the detailed ship hull profile is not needed.A traditional ship maneuvering model is used for the in-plane surge, sway and yaw degrees of freedom with a series of nondimensional coefficients determined from experiments. It is assumed that the out-of-plane degrees of freedom are not coupled with the in-plane ship motions, and there is no coupling among roll, pitch and heave motions. The implementation is verified through free decay tests, and the obtained natural periods show good agreement with theoretical results.Several collision and grounding cases are simulated in which a supply vessel crashes into rigid plates with different orientations. The effects of the roll motion, the heave and pitch motions and the full 6DOF motions are studied. The results are compared with those from a 6DOF decoupled method. Ship motions through the proposed method compare reasonably well with SIMO results. It is found that several consecutive impacts may occur in the simulation of one collision case due to the periodic motions. This is not taken into account in the decoupled method, which makes this method unconservative.     

Can we reliably assess climate mitigation options for air traffic scenarios despite large uncertainties in atmospheric processes?

Air traffic has an increasing influence on climate; therefore identifying mitigation options to reduce the climate impact of aviation becomes more and more important. Aviation influences climate through several climate agents, which show different dependencies on the magnitude and location of emission and the spatial and temporal impacts. Even counteracting effects can occur. Therefore, it is important to analyse all effects with high accuracy to identify mitigation potentials. However, the uncertainties in calculating the climate impact of aviation are partly large (up to a factor of about 2). In this study, we present a methodology, based on a Monte Carlo simulation of an updated non-linear climate-chemistry response model AirClim, to integrate above mentioned uncertainties in the climate assessment of mitigation options. Since mitigation options often represent small changes in emissions, we concentrate on a more generalised approach and use exemplarily different normalised global air traffic inventories to test the methodology. These inventories are identical in total emissions but differ in the spatial emission distribution. We show that using the Monte Carlo simulation and analysing relative differences between scenarios lead to a reliable assessment of mitigation potentials. In a use case we show that the presented methodology can be used to analyse even small differences between scenarios with mean flight altitude variations.