当前位置:主页 > 科技论文 > 航空航天论文 >

基于GNSS的新型位姿一体化确定技术研究

发布时间:2018-08-02 20:43
【摘要】:基于GNSS相对定位,具有低成本,全天候,高精度等优点,在陆、海、空、天领域得到了广泛的应用。同时,基于GNSS姿态确定相比于其它现代姿态测量设备而言,具有价格低廉、维护成本低,且无累计误差等优点,是当前空天导航系统中重点的研究领域。然而,不管是基于GNSS相对定位系统,还是基于GNSS姿态测量系统,通常都是分开处理的。这种分而治之的方式没有考虑到平台和平台之间的基线约束条件,限制了定位和定姿精度的提高。本文深入研究平台多基线限制对定位和定姿的影响,通过对基线限制信息的有效利用,以及综合利用定位和定姿模糊度信息,在提高相对定位精度的同时,提高姿态输出精度。首先,在数据预处理部分,重新设计了天线构型,解决了单平台姿态输出某一姿态误差显著大于另两个姿态误差的问题。同时改进了周跳探测与修复算法,改进后的算法能够对单频、双频和三频信号进行周跳检测和修复。其次,模糊度解算性能的提高。分析了不同星座(GPS、BDS、GPS+BDS)选择对模糊度解算性能的影响。改进搜索收敛法,提高了仿射约束模型姿态模糊度解算性能。同时也分析了限制基线对非限制基线基线估计模糊度解算成功率的影响。最后,对比了AC-AM姿态确定算法、直接姿态确定算法和载波平滑伪距算法姿态输出精度的差异,由于基线限制和算法改进,其精度明显高于前两种姿态确定算法。此外还将姿态确定模块中的模糊度信息引入相对位置解算模块,仿真结果表明引入姿态模糊度信息后,相对定位的精度有了很大的提高。
[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

资料下载
论文发表

本文链接:https://www.wllwen.com/kejilunwen/hangkongsky/2160674.html


Copyright(c)文论论文网All Rights Reserved | 网站地图 |

版权申明:资料由用户967e6***提供,本站仅收录摘要或目录,作者需要删除请E-mail邮箱bigeng88@qq.com