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一种新的低成本组合导航系统初始对准算法
引用本文:岳晓奎,袁建平.一种新的低成本组合导航系统初始对准算法[J].飞行力学,2006,24(2):89-92.
作者姓名:岳晓奎  袁建平
作者单位:西北工业大学,航天学院,陕西,西安,710072
摘    要:基于低成本惯性测量单元的组合导航系统已经逐步成为导航领域的研究热点和主要发展方向。但是,低成本惯性元件精度低,无法进行自主初始对准。基于规范化四元数的概念,研究了一种仅利用GPS的位置和速度数据对组合系统进行初始对准的新算法,克服了传统滤波方法进行初始对准存在的诸多局限性。理论分析和仿真计算表明,这种算法仅受组合系统自身硬件条件的约束,可以较好地应用于组合系统中低成本惯性单元的初始对准。

关 键 词:组合导航  初始对准  四元数法
文章编号:1002-0853(2006)02-0089-04
收稿时间:2005-04-11
修稿时间:2005-12-15

A New Initial Alignment Algorithm for a Low-Cost Integrated Navigation System
YUE Xiao-kui,YUAN Jian-ping.A New Initial Alignment Algorithm for a Low-Cost Integrated Navigation System[J].Flight Dynamics,2006,24(2):89-92.
Authors:YUE Xiao-kui  YUAN Jian-ping
Abstract:A low-cost-inertial-measurement-unit(IMU)based integrated navigation system is already being the research tide in the navigation field.But,because of the limitation of IMU's accuracy,it is impossible to finish its alignment by itself.In this paper,based on the concept of normal quaternion,a new algorithm for the initial alignment of the integrated system is studied;the alignment algorithm is processed only on the basis of the position and velocity data of GPS.Through the correlative theoretic analysis and simulation,this algorithm can be used to finish the initial alignment of the low-cost inertial measurement unit
Keywords:integrated navigation  initial alignment  quaternions
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