| 单频GPS实时定姿系统研究 |
| |
| 引用本文： | 郑冲,周伯昭,吴杰.单频GPS实时定姿系统研究[J].航天控制,2006,24(1):14-18. |
| |
| 作者姓名： | 郑冲 周伯昭 吴杰 |
| |
| 作者单位： | 国防科技大学航天与材料工程学院,长沙,410073 |
| |
| 摘 要： | 介绍了自行研制的单频GPS实时定姿系统硬、软件结构,以及硬件组成和软件设计对GPS定姿系统实时性的影响。然后介绍了定姿系统软件设计过程中对系统可靠性和稳定性的考虑。最后利用该系统完成了GPS实时定姿的静态试验和动态试验。试验表明,系统具有较高的实时定姿精度。该系统可以应用于地面车辆、舰船以及飞行器的姿态确定。
|
| 关 键 词： | 全球定位系统 姿态传感器 整周模糊度 |
| 文章编号： | 1006-3242(2006)01-0014-05 |
| 修稿时间： | 2004年12月6日 |
Research on Single Frequency GPS Real-time Attitude Determination System |
| |
| Zheng Chong,Zhou Bozhao,Wu Jie.Research on Single Frequency GPS Real-time Attitude Determination System[J].Aerospace Control,2006,24(1):14-18. |
| |
| Authors: | Zheng Chong Zhou Bozhao Wu Jie |
| |
| Abstract: | Firstly the hardware,software and real-time performance of a single frequency GPS real-time attitude determination system is introduced in detail.Then the software design to meet the demand of reliability and stability is presented.Finally static and dynamic experiments are carried out and the experiment results show that the system has high precision.It can be used as an attitude sensor on vehicles such as cars,ships and aircrafts. |
| |
| Keywords: | Global Positioning System Attitude Sensor Integer Ambiguity |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
