基于GNSS的新型位姿一体化确定技术研究
[Abstract]:Based on GNSS relative positioning, it has the advantages of low cost, all-weather, high precision, and has been widely used in land, sea, air and sky fields. At the same time, compared with other modern attitude measurement devices, attitude determination based on GNSS has the advantages of low price, low maintenance cost and no accumulated error. However, whether it is based on GNSS relative positioning system or based on GNSS attitude measurement system, it is usually handled separately. This divide-and-conquer approach does not take into account the baseline constraints between the platform and the platform, which limits the accuracy of positioning and attitude determination. In this paper, the effect of multi-baseline limitation on positioning and attitude determination is deeply studied. Through the effective use of baseline restriction information and the comprehensive use of location and attitude ambiguity information, the relative positioning accuracy is improved and the attitude output accuracy is improved at the same time. Firstly, in the part of data preprocessing, the antenna configuration is redesigned to solve the problem that the error of one attitude output from a single platform is significantly larger than that of the other two. At the same time, the cycle slip detection and repair algorithm is improved. The improved algorithm can detect and repair the cycle slip of single frequency, double frequency and three frequency signals. Secondly, the ambiguity resolution performance is improved. The influence of different constellations (GPS BDS BDS) on ambiguity resolution is analyzed. The search convergence method is improved to improve the solution performance of affine constraint model attitude ambiguity. At the same time, the effect of restricted baseline on the success rate of ambiguity resolution in unconstrained baseline estimation is analyzed. Finally, the difference of attitude output accuracy between AC-AM attitude determination algorithm, direct attitude determination algorithm and carrier smoothing pseudo-range algorithm is compared. Because of the baseline limitation and the improvement of the algorithm, the accuracy is obviously higher than that of the first two attitude determination algorithms. In addition, the ambiguity information in the attitude determination module is introduced into the relative position calculation module. The simulation results show that the precision of relative positioning has been greatly improved with the introduction of the attitude ambiguity information.
【学位授予单位】:南京航空航天大学
【学位级别】:硕士
【学位授予年份】:2016
【分类号】:V249.3;V448.2
【参考文献】
相关期刊论文 前10条
1 郑坤;董绪荣;刘亚涛;胡晓粉;;GNSS载波相位多天线实时测姿系统的设计与实现[J];测绘科学技术学报;2014年02期
2 盛汉霖;张天宏;刘冬冬;;基于扩展卡尔曼滤波器的低成本航姿系统设计[J];系统工程与电子技术;2013年10期
3 李建国;崔祜涛;田阳;;基于乘性四元数和约束滤波的飞行器姿态估计算法[J];系统工程与电子技术;2013年05期
4 黄令勇;宋力杰;王琰;智遂强;;北斗三频无几何相位组合周跳探测与修复[J];测绘学报;2012年05期
5 胡庆雷;周稼康;马广富;;无需角速度的含通信时延卫星编队飞行自适应姿态协同跟踪控制[J];自动化学报;2012年03期
6 徐定杰;党超;沈锋;;一种解算整周模糊度几何算法实现GPS快速测姿[J];宇航学报;2011年12期
7 唐大全;毕波;王旭尚;李飞;沈宁;;自主着陆/着舰技术综述[J];中国惯性技术学报;2010年05期
8 孟领坡;吴杰;;基于载波相位的完整性监测及其优化方法[J];遥测遥控;2010年05期
9 滕云龙;师奕兵;郑植;;单频载波相位的周跳探测与修复算法研究[J];仪器仪表学报;2010年08期
10 阳仁贵;袁运斌;欧吉坤;;相位实时差分技术应用于飞行器交会对接研究[J];中国科学:物理学 力学 天文学;2010年05期
相关博士学位论文 前3条
1 陈小平;航天器自主交会对接导航与控制关键技术研究[D];电子科技大学;2012年
2 祖秉法;“北斗二号”民用软件接收机关键技术研究[D];哈尔滨工程大学;2010年
3 唐祖平;GNSS信号设计与评估若干理论研究[D];华中科技大学;2009年
相关硕士学位论文 前1条
1 刘通;基于GPS相对测量的卫星编队碰撞规避研究[D];上海交通大学;2012年
,本文编号:2160674
本文链接:https://www.wllwen.com/kejilunwen/hangkongsky/2160674.html