Semi-physical simulation design for flight control systems based on xPC

WANG Xiao-dong1; DONG Xin-min1; YAO Chong2

doi:10.13873/j.1000-97872011.02.045

Chinese

您当前的位置：

首页 >

文章列表页 >

Semi-physical simulation design for flight control systems based on xPC

更新时间：2025-09-11

- Semi-physical simulation design for flight control systems based on xPC
- Vol. 30, Issue 2, Pages: 122-124(2011)
- 作者机构：
  
  1. 空军工程大学工程学院
  2. 空军第三飞行学院
- 作者简介：
- 基金信息：
- DOI：10.13873/j.1000-97872011.02.045
  CLC： TP273
- Published：2011
- 稿件说明：
移动端阅览
[1]王晓东,董新民,姚崇.基于xPC的飞行控制系统半实物仿真设计[J].传感器与微系统,2011,30(02):122-124.

WANG Xiao-dong1, DONG Xin-min1, YAO Chong2. Semi-physical simulation design for flight control systems based on xPC[J]. 2011, 30(2): 122-124.
[1]王晓东,董新民,姚崇.基于xPC的飞行控制系统半实物仿真设计[J].传感器与微系统,2011,30(02):122-124. DOI： 10.13873/j.1000-97872011.02.045.

WANG Xiao-dong1, DONG Xin-min1, YAO Chong2. Semi-physical simulation design for flight control systems based on xPC[J]. 2011, 30(2): 122-124. DOI： 10.13873/j.1000-97872011.02.045.

摘要

利用Matlab的xPC目标工具在仿真回路中引入飞控计算机、传感器等实物部件

设计了某型飞机飞行控制系统的半实物仿真系统。根据飞行控制系统的原理特点设计了数据采集卡与信号转换处理电路

并在VC6.0环境下对系统软件进行了编制。仿真结果表明:该半实物仿真系统具有较高的仿真置信度和可靠度。

Abstract

With the introduction of flight control computers

sensors and other physical components to the simulation loop

semi-physical simulation system of an type of aircraft is designed by xPC target tool of Matlab.Data acquisition card and signal transition and processing circuit are designed according to the principles and characteristics of flight control system.System software is programmed under VC 6.0.Simulation result shows that the semi-physical simulation system has high confidence level.

关键词

Keywords

references

VxWorks下飞行模拟系统研究与设计 [J]. 汪旭光,袁冬莉,闫建国. 飞行力学 . 2008(02)

基于xPC目标的实时I/O接口技术研究 [J]. 宋炜,祖家奎. 自动化技术与应用 . 2008(01)

某型无人直升机飞控系统仿真研究 [J]. 陈巍,王道波. 飞行力学 . 2004(01)

半实物仿真[M]. 国防工业出版社 , 单家元, 2008

系统实时仿真开发环境与应用[M]. 清华大学出版社 , 杨涤等编著, 2002

Views

290

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Design of micro UAV flight control system based on SOPC

Design of attitude determination and control system of high subsonic UAV flight

Related Author

SONG Yu

SONG Jun-wei

PU Huang-zhong1

ZHEN Zi-yang1

WANG Dao-bo1

HU Yong2

Related Institution

College of Computer Science and Engineering,Changchun University of Technology

College of Automation Engineering,Nanjing University of Aeronautics and Astronautics

College of Electrical Engineering,Zhejiang University

⁰