| 组合导航系统快速原型设计 |
| |
| 引用本文： | 殷红珍,唐硕,黄勇,泮斌峰. 组合导航系统快速原型设计[J]. 计算机辅助工程, 2008, 17(3): 45-48 |
| |
| 作者姓名： | 殷红珍 唐硕 黄勇 泮斌峰 |
| |
| 作者单位： | 1. 西北工业大学,航天学院,西安,710072
2. 北京航空航天大学,自动化科学与电气工程学院,北京,100083 |
| |
| 摘 要： | 为加快捷联惯性导航/卫星定位组合导航系统（Strapdown Inertial Navigation System/Global Positioning System,SINS/GPS）从算法到硬件产品的实现过程,采用快速原型技术进行设计.该方法在1个统一的Matlab/Simulink开发环境中建立系统模型并进行数字仿真;借助RT-LAB快速原型开发平台和实时工作间（Real-Time Workshop,RTW）为系统模型自动生成代码并加载到目标机和DSP硬件;实现SINS/GPS组合导航系统DSP硬件在回路仿真的快速原型设计.系统实时仿真结果与数字仿真结果一致,表明其具有开发周期短、实时性能好等优点.
|
| 关 键 词： | 组合导航 数字信号处理器 快速原型 代码自动生成技术 MATLAB SIMULINK 实时工作间 |
| 收稿时间： | 2007-12-04 |
| 修稿时间： | 2008-01-02 |
Rapid prototype design on integrated navigation system |
| |
| YIN Hongzhen,TANG Shuo,HUANG Yong and PAN Binfeng. Rapid prototype design on integrated navigation system[J]. Computer Aided Engineering, 2008, 17(3): 45-48 |
| |
| Authors: | YIN Hongzhen TANG Shuo HUANG Yong PAN Binfeng |
| |
| Affiliation: | YIN Hongzhen1,TANG Shuo1,HUANG Yong2,PAN Binfeng1(1.School of Astronautics,Northwestern Polytechnical Univ.,Xi'an 710072,China,2.School of Automation Sci.& Electronical Eng.,Beijing Univ.of Aeronautics & Astronautics,Beijing 100083,China) |
| |
| Abstract: | To accelerate the development of Strapdown Inertial Navigation System/Global Positioning System(SINS/GPS)products from algorithm to hardware,the rapid prototype technology is used to design the system.The system model is designed and the digital simulation is done in a unified development environment of Matlab/Simulink.The code is automatically generated for the system model and loaded on the target machine and DSP hardware by using the rapid prototype development platform RT-LAB and Real-Time Workshop(RTW)... |
| |
| Keywords: | Matlab Simulink |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《计算机辅助工程》浏览原始摘要信息 |
|
点击此处可从《计算机辅助工程》下载全文 |
|
