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双天线测向信息辅助捷联惯导快速对准算法
引用本文:刘俊杰,陈 健,贾继超,商 阳. 双天线测向信息辅助捷联惯导快速对准算法[J]. 测控技术, 2021, 40(1): 110-113. DOI: 10.19708/j.ckjs.2021.01.018
作者姓名:刘俊杰  陈 健  贾继超  商 阳
作者单位:航空工业陕西飞机工业(集团)有限公司,陕西汉中 723200;航空工业陕西飞机工业(集团)有限公司,陕西汉中 723200;中国航天科技集团公司第九研究院第十六研究所,陕西西安 710100;航空工业西安飞行自动控制研究所,陕西西安 710076
摘    要:为解决捷联惯导的快速高精度对准问题,给出了一种双天线测向信息辅助的惯导快速对准算法.介绍了双天线测向的基本原理,在此基础上给出了双天线基线安装误差的补偿方法.基于速度、位置、航向观测量,设计了快速对准卡尔曼滤波器,给出了具体航向量测方程.根据实测双天线测向误差特性进行了仿真分析.仿真结果验证了方法的有效性,4 min航...

关 键 词:捷联惯导  双天线测向  快速对准  卡尔曼滤波

A Fast Alignment Algorithm for Strapdown Inertial Navigation Aided by Dual Antenna Orientation
LIU Jun-jie,CHEN Jian,JIA Ji-chao,SHANG Yang. A Fast Alignment Algorithm for Strapdown Inertial Navigation Aided by Dual Antenna Orientation[J]. Measurement & Control Technology, 2021, 40(1): 110-113. DOI: 10.19708/j.ckjs.2021.01.018
Authors:LIU Jun-jie  CHEN Jian  JIA Ji-chao  SHANG Yang
Abstract:In order to solve the problem of fast and high precision alignment of strapdown inertial navigation,a fast inertial navigation alignment algorithm aided by dual antenna orientation is proposed.The basic principle of dual antenna orientation was described,and the compensation method for dual antenna baseline installation error was presented.The fast alignment Kalman Filter was designed based on the measurements of speed,position and heading,and the specific vector survey equation was derived,and simulation analysis was performed.The result proves this method to be effective with 4 min heading accuracy better than 0.05°,which can meet the alignment accuracy requirement of common 0.8 nm/h airborne strapdown inertial system.The dual antenna orientation alignment algorithm is much faster than the traditional compass-based speed and position measurement and alignment methods,but the specific alignment heading accuracy is affected by the error of the dual antenna direction greatly.
Keywords:strapdown inertial navigation  dual antenna orientation  fast alignment  Kalman Filter
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