| 球载捷联惯性/GPS组合导航系统及动态对准技术 |
| |
| 引用本文： | 张音,李星海,李勇建.球载捷联惯性/GPS组合导航系统及动态对准技术[J].华南农业大学学报(社会科学版),2010(5). |
| |
| 作者姓名： | 张音 李星海 李勇建 |
| |
| 作者单位： | 张音(南京电子技术研究所,南京,210039);李星海,李勇建(四川压电与声光技术研究所,重庆,400060)? |
| |
| 摘 要： | 为了实现系留气球载雷达系统天线的空域稳定,球载航姿系统是不可缺少的重要设备.文中阐述了用捷联惯性/全球定位系统组合导航系统实现球载航姿系统的设计技术,针对系留气球平台系统在空中漂浮不定的特点,提出了在动态条件下,小型系留气球载捷联惯性/GPS组合导航系统的对准技术.
|
| 关 键 词： | 组合导航系统 捷联惯性系统 全球定位系统 卡尔曼滤波 数字信号处理 |
Aerostat-Borne Strapdown Inertial/GPS Integrated Navigation System and Alignment Technique at Dynamic State |
| |
| ZHANG Yin,LI Xing-hai,LI Yong-jian.Aerostat-Borne Strapdown Inertial/GPS Integrated Navigation System and Alignment Technique at Dynamic State[J].Journal of South China Agricultural University:Social Science Edition,2010(5). |
| |
| Authors: | ZHANG Yin LI Xing-hai LI Yong-jian |
| |
| Institution: | ZHANG Yin1,LI Xing-hai2,LI Yong-jian2 (1. Nanjing Research Institute of Electronics Technology,Nanjing 210039,China) (2. Sichuan Institute of Piezoelectric & Acoustooptic Technology,Chongqing 400060,China) |
| |
| Abstract: | In order to realize the airspace stabilization of the antenna of a tethered aerostat-borne radar system,the tethered aerostat-borne navigation attitude system is an absolute necessarily important equipment. The design technique is proposed in this paper that utilizes the strapdown inertial/GPS integrated navigation system to realize the tethered aerostat-borne navigation attitude system. Aiming at the floating characteristic of the tethered aerostat-borne system,an alignment technique of miniaturized tether... |
| |
| Keywords: | integrated navigation system strapdown inertial system GPS kalman filter DSP |
|
| 点击此处可从《华南农业大学学报(社会科学版)》浏览原始摘要信息 |
| 点击此处可从《华南农业大学学报(社会科学版)》下载免费的PDF全文 |
