航空兵器Issue(5)：18-24,7.DOI:10.19297/j.cnki.41-1228/tj.2016.050.04
差分 GPS／S INS 超紧组合在线标定与误差补偿方案设计
Design of Online Calibration andError Compensation of Differential GPS/SINS Ultra-Tight I ntegration
摘要
Abstract
In order to further improve the navigation accuracy and error calibration accuracy of the GPS/SINS ultra-tight integrated system , a scheme for GPS/SINS ultra-tight integrated navigation system based on carrier phase difference is proposed .On the one hand ,by aiding GPS tracking loop with the SINS, the carrier loop noise bandwidth and the code correlator spacing are reduced , the tracking precision of carrier ring and code loop are improved.On the other hand , the high precision measurement informa-tion is provided as integrated navigation measurement by carrier phase , which can accurately calibrate and compensate the IMU error .The navigation accuracy of GPS S/INS ultra-tight integrated system is improved further .关键词
捷联惯性导航系统/全球定位系统/载波相位差分/在线标定/误差补偿Key words
SINS/GPS/carrier phase difference/online calibration/error compensation分类
航空航天引用本文复制引用
葛俊,王新龙,车欢,李群生..差分 GPS／S INS 超紧组合在线标定与误差补偿方案设计[J].航空兵器,2016,(5):18-24,7.基金项目
航空科学基金项目（20130151004；2015ZC51038）；卫星应用研究院创新基金项目2 （）
