| 基于GPS的直升机航迹测量系统 |
| |
| 引用本文： | 韩玉旺,郝宗敏.基于GPS的直升机航迹测量系统[J].直升机技术,2009(3). |
| |
| 作者姓名： | 韩玉旺 郝宗敏 |
| |
| 作者单位： | 中国直升机设计研究所,景德镇,333001 |
| |
| 摘 要： | 基于GPS直升机航迹测量系统是利用高精度的GPS实时RTK、逆向RTK和事后动态载波相位差分技术,用于直升机飞行试验中的航迹、速度、高度等信息的测量和实时显示。同时系统融合了高速无线数字通讯技术、惯导设备等多种高新技术。
|
| 关 键 词： | GPS 载波相位差分 直升机航迹 实时监控 |
Helicoptor Flight Path Measurement System Based on GPS |
| |
| Authors: | HAN Yuwang HAO Zongmin |
| |
| Institution: | HAN Yuwang; HAO Zongmin(China Helicopter Research and Development Institute; Jingdezhen; 333001); |
| |
| Abstract: | Helicoptor flight path measurement system based on GPS,which uses high précised-GPS real-time RTK,anti-direction RTK and dynamic Carrier Wave Phasic Difference technology,is used for measurement and real-time display of track,velocity,attitude information during helicopter flight test.The system adopts many technologies such as high-speed digital communication technology,habitual navigation equipment,etc. |
| |
| Keywords: | GPS |
| 本文献已被 维普 万方数据 等数据库收录！ |
|
