首页 | 本学科首页   官方微博 | 高级检索  
     检索      

多约束条件的全球定位系统单频单历元短基线定向技术与实现
引用本文:任光辉,茅旭初.多约束条件的全球定位系统单频单历元短基线定向技术与实现[J].上海交通大学学报,2014,48(3):335-340.
作者姓名:任光辉  茅旭初
作者单位:(上海交通大学 电子信息与电气工程学院,上海 200240)
摘    要:通过研究全球定位系统(GPS)伪距测量精度对GPS载波相位差分技术在短基线定向问题中的影响,提出利用基线长度、基线俯仰、卫星之间几何关系的多约束最小二乘整周模糊度实时搜索算法,给出单频单历元进行短基线定向的具体过程和需要注意的关键问题.算法采用单历元解算,规避载波相位周跳问题,极大地减小初始化时间.静态和动态实验结果均表明:该方法快速有效,解算成功率高,具有较高的定向精度.

关 键 词:全球定位系统    卫星导航    单频单历元    基线约束    整周模糊度    最小二乘搜索  
收稿时间:2013-04-01

Single Frequency and Single Epoch Short Baseline GPS Orientation Determination Method and Realization with Multiple Constraints
REN Guang-hui;MAO Xu-chu.Single Frequency and Single Epoch Short Baseline GPS Orientation Determination Method and Realization with Multiple Constraints[J].Journal of Shanghai Jiaotong University,2014,48(3):335-340.
Authors:REN Guang-hui;MAO Xu-chu
Institution:(School of Electronic and Electric Engineering, Shanghai Jiaotong University Shanghai 200240, China)
Abstract:Satellite orientation, as one of the main technologies in modern navigation field, has many advantages, such as low cost, quick initialization, high precision and no accumulate error. Based on the discussion of the effect between the accuracy of pseudo-range and carrier phase in the short baseline orientation determination, an improved least squares real-time search algorithm was proposed, which had multi-constraints with fixed baseline length, known pitch angle and geometric relationship among visual satellites. Because of using single epoch information only, the method avoided carrier phase cycle slips, which reduced the initial time significantly. The static and dynamic experimental results proved that this method is speedy and efficient, which is characterized by high success rate and high accuracy in the orientation determination.
Keywords:global positioning system  satellite navigation  single frequency and single epoch  baseline constraint  integer ambiguity  least squares search  
本文献已被 CNKI 等数据库收录!
点击此处可从《上海交通大学学报》浏览原始摘要信息
点击此处可从《上海交通大学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号