| 一种惯性/GPS伪距/伪距率组合导航算法 |
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| 引用本文： | 王黎斌,尚克军,王孝利,周祖洋. 一种惯性/GPS伪距/伪距率组合导航算法[J]. 战术导弹控制技术, 2011, 0(1) |
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| 作者姓名： | 王黎斌 尚克军 王孝利 周祖洋 |
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| 作者单位： | 北京自动化控制设备研究所; |
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| 摘 要： | 紧组合技术是当前惯性/卫星组合导航技术的发展趋势,而惯性/卫星伪距/伪距率组合导航算法是紧组合技术的基本算法。本文提出了一种惯性/卫星伪距/伪距率的组合导航算法的实现方法,并采用惯导和接收机的动态数据进行了离线仿真,仿真结果表明,本文提出的伪距/伪距率的组合导航算法直接采用接收机测量的伪距、伪距率信息作为观测量,能够准确估计惯导误差,消除了量测输入的相关性问题,尤其是在GPS卫星数为2时仍能保持较高的导航精度,为惯性/卫星紧组合技术的进一步研究奠定了基础。
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| 关 键 词： | 紧组合 伪距/伪距率组合 |
A INS/GPS integrated navigation method in pseudo range and pseudo range rate |
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| WANG Li-bin,SHANG Ke-jun,WANG Xiao-li,ZHOU Zu-yang. A INS/GPS integrated navigation method in pseudo range and pseudo range rate[J]. Control Technology of Tactical Missile, 2011, 0(1) |
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| Authors: | WANG Li-bin SHANG Ke-jun WANG Xiao-li ZHOU Zu-yang |
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| Affiliation: | WANG Li-bin,SHANG Ke-jun,WANG Xiao-li,ZHOU Zu-yang(Beijing Institute of Automatic Control Equipment,Beijing 100074,China) |
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| Abstract: | A INS/GPS integrated navigation method in pseudo range and pseudo range rate is basic in tight-integrated technology which is a trend in the field of INS/GPS integrated navigation now.In this article,a INS/GPS integrated navigation method in pseudo range and pseudo range rate is proposed,by which the data from a INS and a GPS receiver is simulated off-line.The result shows that,the method can nicely estimate INS error with the raw information of pseudo range and pseudo range rate from a GPS receiver,and can... |
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| Keywords: | tight-integrated technology a integrated navigation method in pseudo range and pseudo range rate |
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