首页 | 本学科首页   官方微博 | 高级检索  
     

基于低成本接收机的双天线测姿算法
引用本文:王守华,李云柯,孙希延,纪元法.基于低成本接收机的双天线测姿算法[J].计算机应用,2019,39(8):2381-2385.
作者姓名:王守华  李云柯  孙希延  纪元法
作者单位:广西精密导航技术与应用重点实验室(桂林电子科技大学),广西桂林541004;卫星导航定位与位置服务国家地方联合工程研究中心,广西桂林541004;广西精密导航技术与应用重点实验室(桂林电子科技大学),广西桂林541004;卫星导航定位与位置服务国家地方联合工程研究中心,广西桂林541004;广西精密导航技术与应用重点实验室(桂林电子科技大学),广西桂林541004;卫星导航定位与位置服务国家地方联合工程研究中心,广西桂林541004;广西精密导航技术与应用重点实验室(桂林电子科技大学),广西桂林541004;卫星导航定位与位置服务国家地方联合工程研究中心,广西桂林541004
基金项目:国家重点研发计划项目(2018YFB0505103);国家自然科学基金资助项目(61561016,11603041);广西自然科学基金资助项目(2018GXNSFAA050123);广西精密导航技术与应用重点实验室主任基金资助项目(DH201803);桂林电子科技大学研究生教育创新计划项目(2018YJCX28,2019YCXS037);广西科技厅项目(桂科AA17202033)。
摘    要:针对低成本接收机双天线测姿系统利用直接法解算精度较低且存在系统粗差的问题,提出一种基于载波和伪距双差实时动态定位(RTK)卡尔曼滤波算法。首先,引入基线长度作为观测量,并将事先测量得到的精确基线长度作为观测量误差;然后,根据从天线接收机的历元时间间隔对主天线位置进行实时矫正,而周整模糊度采用改进LABMDA算法求解。在静态和动态情况下进行了测试,结果表明,在基线长度为1.1m、采用GPS和北斗双系统进行观测的情况下,所提算法解算出的航向角精度在1°左右,俯仰角精度在2°~3°。相比传统的双天线直接法测姿,该算法在系统抗差性能和精度上都较优。

关 键 词:双天线测姿  低成本接收机  卡尔曼滤波  基线约束  实时动态定位
收稿时间:2018-12-27
修稿时间:2019-03-11

Dual-antenna attitude determination algorithm based on low-cost receiver
WANG Shouhua,LI Yunke,SUN Xiyan,JI Yuanfa.Dual-antenna attitude determination algorithm based on low-cost receiver[J].journal of Computer Applications,2019,39(8):2381-2385.
Authors:WANG Shouhua  LI Yunke  SUN Xiyan  JI Yuanfa
Affiliation:1. Guangxi Key Laboratory of Satellite Navigation and Location Awareness(Guilin University of Electronic Technology), Guilin Guangxi 541004, China;2. National and Local Joint Engineering Research Center of Satellite Navigation and Location Awareness, Guilin Guangxi 541004, China
Abstract:Concerning the problem that low-cost Dual-antenna Attitude determination System (DAS) has low accuracy and gross error because of using direct solution, an improved algorithm based on carrier phase and pseudo-range double-difference Real-Time Kinematic (RTK) Kalman filter was proposed. Firstly, the baseline length was employed as the observation, then the precise baseline length obtained in advance was taken as the observation error. Secondly, the position of master antenna was corrected according to the epoch time interval of the slave antenna receiver and the integer ambiguity was solved by MLABMDA (Modified LABMDA) algorithm. Experimental results in static and dynamic mode show that the accuracy of the heading angle calculated by the proposed algorithm is about 1 degree and the calculated pitch angle accuracy is about 2-3 degrees in the case of baseline length 1.1 m with GPS and Beidou dual systems. The proposed algorithm improves the robustness and accuracy of the system greatly compared with the traditional dual-antenna attitude determination by direct solution.
Keywords:dual-antenna attitude determination                                                                                                                        low-cost receiver                                                                                                                        Kalman filter                                                                                                                        baseline constraint                                                                                                                        Real Time Kinematic (RTK)
本文献已被 维普 万方数据 等数据库收录!
点击此处可从《计算机应用》浏览原始摘要信息
点击此处可从《计算机应用》下载全文
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