Conceptual design and RCS performance research of shipborne early warning aircraft

In order to improve the survivability of the aircraft,conceptual design and radar cross section（RCS） performance research are done. The CATIA software is used to design the 3D digital model of the shipborne early warning aircraft, and some measures are taken to reduce the RCS characteristics of the early warning aircraft at the same time. Based on the physical optics method and the equivalent electromagnetic flow method,the aircraft＇s RCS characteristics and strength distribution characteristics are simulated numerically, and compared with the foreign advanced shipborne early warning aircraft. The simulation results show that under the X radar band, when the incident wave pitching angle is 0？, compared with the foreign advanced shipborne early warning aircraft, the forward RCS average value of the conceptual shipborne early warning aircraft is reduced to 24.49%, the lateral RCS average value is reduced to 5.04%, and the backward RCS average value is reduced to 39.26%. The research results of this paper are expected to provide theoretical basis and technical support for the conceptual design and the stealth design of the shipborne early warning aircraft.     

高速列车模拟器的视景建模与仿真

高速列车模拟器是培训高速列车司机的先进工具。本文介绍了高速列车模拟器中视景仿真系统的开发，对视景仿真系统构成，视景仿真软件的开发，场景模型的建立进行了研究，并给出了适合于沿铁路轨道进行视点计算的数据结构。     

Consensus intuitionistic fuzzy group decision-making method for aircraft cockpit display and control system evaluation

A novel group decision-making (GDM) method based on intuitionistic fuzzy sets (IFSs) is developed to evaluate the ergonomics of aircraft cockpit display and control system (ACDCS). The GDM process with four steps is discussed. Firstly, approaches are proposed to transform four types of common judgement representations into a unified expression by the form of the IFS, and the features of unifications are analyzed. Then, the aggregation operator called the IFSs weighted averaging (IFSWA) operator is taken to synthesize decision-makers’ (DMs’) preferences by the form of the IFS. In this operator, the DM’s reliability weights factors are determined based on the distance measure between their preferences. Finally, an improved score function is used to rank alternatives and to get the best one. An illustrative example proves the proposed method is effective to valuate the ergonomics of the ACDCS.     

RDSS卫星授时误差建模与仿真测试

RDSS定时终端在不同领域得到广泛应用,终端技术取得日新月异的变化,但是由于RDSS体制的特殊性,相关信号模拟器的国内研制相对滞后,不具备仿真功能,无法满足定时终端定时处理流程和算法的测试需求.因此,研制具有仿真模型的模拟器支持调试研发是当前终端测试的迫切需求.本文详述了基于RDSS卫星授时的原理,分析了动态信号的模拟要求,建立了卫星转发时刻、卫星轨道参数、目标运动轨迹、信号传输误差等仿真模型.信号源实测数据表明,各项指标满足测试需求.     

基于PC104总线的航电模拟器设计与实现

针对飞行器飞控系统试验中对航电设备的仿真需求,设计了基于PC104总线架构的航电模拟器,其性能可靠,而且扩展方便,易于实现较强的航电信号仿真功能,同时其结构紧凑,适合便携式仪器设计.作为一个应用实例,详细阐述了整个系统的框架结构及相应的软、硬件设计思路,并在此基础上给出了部分原理图.     

燃气轮机启动电机负载模拟系统

为了更好地研究燃气轮机启动电动机的启动特性,给出了一种45kW燃气轮机启动电动机负载特性模拟系统,介绍了系统的组成,工作原理以及硬件、软件的设计方案.试验结果表明系统具有良好的动静态性能,能够很好地模拟燃气轮机启动电动机的启动特性.对其他类似的负载模拟系统具有一定的参考价值.     

直升机飞行模拟器及其特点

根据直升机与固定翼飞机飞行方式、操纵方式和任务使命的不同,简单叙述了直升机地面飞行模拟器研制的一般要求和特殊要求,并讨论了直升机飞行仿真模型的部件建模方法,特别是诱导速度模型和机身模型的特殊建模方法.最后给出了典型直升机地面飞行模拟器的飞行模拟曲线、分析以及飞行员评价,验证了模拟效果的可信性.     

电网培训仿真器中图形支撑平台的应用探讨

图形用户界面是电网培训仿真器不可缺少的一部分，为减少图形系统的重复开发，构建一个图形支撑平台十分必要。本文在分析了传统的图形系统设计中的不足后，确定了电网培训仿真系统（DTS）中图形支撑平台的系统结构和设计原则，充分考虑了平台的一致性、开放性、独立性、容错性等，系统地讨论了图形支撑平台的主要内容及实现方法，包括图形编辑模块、教员／学员机图形显示系统、图形的打印等，介绍的方案已成功应用于实际的电网调度员培训仿真系统中。     

高动态飞行器姿态解算及三维视景仿真研究

建立了高动态飞行器姿态解算的数学模型,探讨了利用等效旋转矢量法解算姿态角的方法,并与四元数法进行了比较。建立了飞行器、地形、地物的三维模型,利用计算出来的数据进行飞行器的实时三维视景仿真模拟。三维视景仿真对直接观察、验证高动态飞行器的运动变化规律提供了极大的便利。     

轮机模拟器船舶柴油机改进的仿真软件

介绍轮机模拟器船舶柴油机改进的仿真软件.首先,对6S60MC柴油机工作过程数学建模,包括气缸、涡轮增压器、空冷器、扫气过程和排气过程等;其次,采用一种改进的方法计算排气过程,在满足计算精度要求的同时,缩短工作过程仿真的计算时间;第三,计算柴油机各缸的主要工作参数,比如,示功图P-ψ,P-V和T-ψ,dQ/dψ-ψ,dx/dψ-ψ等曲线图,以及扫气空气系数、残余废气系数、燃烧室壁温等参数;第四,软件有许多故障设置,以训练学生或学员判断故障的能力;第五,软件还有报警参数等.