某型直升机飞行性能仿真建模与验证

主要研究并建立直升机飞行性能仿真模型,在直升机动力学和运动学微分方程的基础上重点解算作用在直升机各部件上的气动力和力矩模型,建立旋翼和尾桨的气动仿真模型,对旋翼挥舞运动进行了分析研究,还考虑了平尾、垂尾、机身和重力的仿真模型。最后通过对各飞行性能指标及其验证原理方法的分析研究,验证了静态性能指标,应用标量指标法验证动态性能指标。     

基于加权LS-SVM的飞行事故率预测模型

飞行事故率是表征飞行安全水平的重要指标,其预测是典型的小样本问题。针对飞行事故率预测建模难的问题,采用加权LS-SVM方法,建立了飞行事故率的时间序列预测模型。仿真实验表明,加权LS-SVM具有很高的建模精度和较强的泛化能力,从而验证了该方法的有效性和先进性。     

Two-step design of critical control systems using disturbance cancellation integral controllers

An efficient critical control system design is proposed in this paper. The key idea is to decompose the design problem into two simpler design steps by the technique used in the classical loop transfer recovery method (LTR). The disturbance cancellation integral controller is used as a basic controller. Since the standard loop transfer recovery method cannot be applied to the disturbance cancellation controller, the nonstandard version recently found is used for the decomposition. Exogenous inputs with constraints both on the amplitude and rate of change are considered. The majorant approach is taken to obtain the analytical sufficient matching conditions. A numerical design example is presented to illustrate the effectiveness of the proposed design.     

An improved new error estimation algorithm for optimal filter lengths for stereophonic acoustic echo cancellation

In this paper, we propose an new error estimate algorithm (NEEA) for stereophonic acoustic echo cancellation (SAEC) that is based on the error estimation algorithm (EEA) in [Nguyen-Ky T, Leis J, Xiang W. An improved error estimate algorithm for stereophonic acoustic echo cancellation system. In: International conference on signal processing and communication systems, ICSPCS’2007, Australia; December 2007]. In the EEA and NEEA, with the minimum error signal fixed, we compute the filter lengths so that the error signal may approximate the minimum error signal. When the echo paths change, the adaptive filter automatically adjusts the filter lengths to the optimum values. We also investigate the difference between the adaptive filter lengths. In contrast with the conclusions in [Khong AWH, Naylor PA. Stereophonic acoustic echo cancellation employing selective-tap adaptive algorithms. IEEE Trans Audio, Speech, Lang Process 2006;14(3):785-96, Gansler T, Benesty J. Stereophonic acoustic echo cancellation and two channel adaptive filtering: an overview. Int J Adapt Control Signal Process 2000;4:565-86, Benesty J, Gansler T. A multichannel acoustic echo canceler double-talk detector based on a normalized cross-correlation matrix. Acoust Echo Noise Control 2002;13(2):95-101, Gansler T, Benesty J. A frequency-domain double-talk detector based on a normalized cross-correlation vector. Signal Process 2001;81:1783-7, Eneroth P, Gay SL, Gansler T, Benesty J. A real-time implementation of a stereophonic acoustic echo canceler. IEEE Trans. Speech Audio Process 2001;9(5):513-23, Gansler T, Benesty J. New insights into the stereophonic acoustic echo cancellation problem and an adaptive nonlinearity solution. IEEE Trans. Speech Audio Process 2002; 10(5):257-67, Benesty J, Gansler T, Morgan DR, Sondhi MM, Gay SL. Advances in network and acoustic echo cancellation. Berlin: Springer-Verlag; 2001], our simulation results have shown that the filter lengths can be different. Our simulation results also confirm that the NEEA is better than EEA and SM-NLMS algorithm in terms of echo return loss enhancement.     

iNET的技术框架和应用前景

简要介绍了iNET（增强遥测综合网）的概念、国外的iNET项目计划及iNET的技术路线。重点讨论了iNET的技术框架,包括iNET的体系结构、遥测网络系统、外围设备、外设配置人机接口、网络管理和频谱资源管理等组成部分和iNET的主要功能,探讨了iNET的目标和在航空飞行试验中的应用前景。     

LabVIEW FPGA模块在飞控计算机测试系统中的应用

飞控计算机是战术飞行武器控制系统的核心。针对其接收发送数字信号的不同时序要求,利用LabVIEW FPGA模块生成飞控计算机测试系统中的测试激励信号,同时接收其数字输出响应,完成测试。详细介绍了LabVIEW FPGA模块的硬件接口设计与软件设计,实践表明应用LabVIEW FPGA模块能缩短系统开发周期,系统可靠性高,工作稳定,满足设计要求。     

新一代遥测网络系统——TmNS

遥测网络系统（TmNS）是增强遥测综合网（iNET）的核心组成部分。概述了遥测网络系统（TmNS）的概念与范畴,探讨了遥测网络系统的技术框架,包括系统组成、体系结构、增强功能和主要技术指标,并给出了一种可行的TmNS技术实现方案。     

一种高效的QMC检测算法

基于垂直分层空时码的MIMO-OFDM系统提出一种高效的QMC检测算法,该算法对信道矩阵进行一次排序QR分解,对最先检测的信号层采用ML-OSIC算法,用M算法检测中间的信号层,逐层增加保留值M以提高算法有效性,利用串行干扰消除检测余下的信号层。与QRD-M算法相比,QMC检测算法能降低计算复杂度。仿真结果表明,该算法以更低的计算复杂度获得更接近最大似然检测的性能,取得性能与复杂度之间的折中更理想。     

一种高逼真度的控制显示组件仿真方法

为增强飞行员对控制显示组件(CDU)的直观感受,提高CDU仿真的逼真度,基于嵌入式PC104 CPU和8255可编程设备接口卡,设计仿真键盘硬件电路和键盘码扫描程序,实现对CDU键盘的高逼真硬件仿真。利用面向对象仿真技术,创建出CDU仿真页面,有效解决了页面系统繁重的生成与管理问题。仿真实验结果表明,该方法能够逼真地实现对飞行计算航路数据和性能参数的输入与显示。     

运输机起飞性能试飞测试技术

运输机进行局部改装后,其结构和气动外形发生了变化.起飞性能是飞行试验中一项重要考核项目,通过构建基于地面光电测试和机载影像测试的综合测试系统,对飞机起飞过程中一台发动机停车情况下的两种处理方式(即中断起飞和继续起飞)进行试飞测试,精确获取飞机的运动参数.通过对实测参数、运动影像以及机载信号量等信息比对分析,得出试验结果...