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两种多天线GNSS动态定姿方法的比较
引用本文:蔡小波,许厚泽,柴华,丁磊香,王勇.两种多天线GNSS动态定姿方法的比较[J].导航与控制,2017(6):14-18.
作者姓名:蔡小波  许厚泽  柴华  丁磊香  王勇
作者单位:1. 中国科学院测量与地球物理研究所大地测量与地球动力学国家重点实验室,武汉430077;中国科学院大学, 北京100049;2. 中国科学院测量与地球物理研究所大地测量与地球动力学国家重点实验室,武汉,430077
基金项目:国家自然科学基金(编号:41274084)
摘    要:针对移动载体对姿态的需求,对两种多天线GNSS动态定姿方法,即直接法和最小二乘迭代法进行了研究.分析了定姿的原理,给出了姿态解算模型.基于车载四天线GNSS的实测数据,分别用两种方法进行了姿态解算,并用同一运动平台高精度惯导给出的姿态作为参考值,对两种定姿方法的精度和可靠性进行了分析和比较.

关 键 词:多天线GNSS  动态定姿  基线  最小二乘迭代

The Comparison of Two Dynamic Attitude Determination Methods Based on Multi-antenna GNSS
CAI Xiao-bo,XU Hou-ze,CHAI Hu,DING Lei-xiang and WANG Yong.The Comparison of Two Dynamic Attitude Determination Methods Based on Multi-antenna GNSS[J].Navigation and Control,2017(6):14-18.
Authors:CAI Xiao-bo  XU Hou-ze  CHAI Hu  DING Lei-xiang and WANG Yong
Abstract:In view of the demands of attitude in mobile systems, two attitude determination methods based on the multi-antenna global navigation satellite system(GNSS), the direct method and the least square iterative method are researched. The principles of the attitude determination are analyzed and the models are derived. The data from a test on a land vehicle which used four-antenna are processed by the two methods. The attitude from a high accuracy inertial navigation system(INS) on the same platform is used as reference, and the accuracy and reliability of the two attitude determination methods are evaluated and compared.
Keywords:multi-antenna GNSS  dynamic attitude determination  baseline  the least square iterative
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