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ENGINEERING REALIZATION OF MULTIPLE ANTENNA GPS IN ATTITUDE DETERMINATION INTEGRATED SYSTEM

姿态确定组合系统中多天线GPS的工程实现(英文)
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摘要 A multiple antenna GPS system integrated with MEMS-based INS is proposed by data fusion. The system is applied to attitude determination due to its high accuracy, the high output rate, low latency, quick initialization, and good robustness and redundancy. The mathematical method for realizing the system is given. The system can provide attitude and other navigation information even without GPS measurement for a period of time. Experimental results show that, under the condition of 200 Hz, the attitude, the position, the velocity, the acceleration, and the angular rate can achieve 0. 08°/s, 1.5 m, 0. 1 m/s, 0. 12 m/s^2 and 0. 1°/s. 设计了一种具有高精度姿态确定性能,高输出率、低耗、快速初始化、通过数据合成而具备坚固性和冗余性的多天线GPS和微机械惯导组合的姿态确定系统。给出了实现该系统的数学方法。该系统在一段时间内没有GPS测量信息也能提供姿态以及其他的导航信息。试验结果表明在200Hz状态下姿态、位置、速度、加速度以及角速率可以达到0.08°/s、1.5m、0.1m/s、0.12m/s2和0.1°/s。
作者 王玫 张炎华
出处 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2006年第4期283-290,共8页 南京航空航天大学学报(英文版)
关键词 multiple antenna attitude determination NAVIGATION rotation matrix 多天线 姿态确定 导航 转换矩阵
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