首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于横向地球坐标的惯性导航方法
引用本文:王海波,张汉武,张萍萍,王军,郝勇帅.基于横向地球坐标的惯性导航方法[J].中国惯性技术学报,2016(6):716-722.
作者姓名:王海波  张汉武  张萍萍  王军  郝勇帅
作者单位:1. 海军大连舰艇学院航海系,大连,116018;2. 海军大连舰艇学院航海系,大连116018;海军大连舰艇学院研究生管理大队,大连116018;3. 海军大连舰艇学院研究生管理大队,大连,116018;4. 海军大连舰艇学院导弹系,大连,116018
基金项目:国防科研基金(DJYKY2014-077)
摘    要:针对极区经线迅速收敛于极点造成的传统惯导机械编排在极区不适用问题,提出了CGCS2000地球椭球体模型下基于横向地球坐标的惯性导航方法。在构建横向坐标系及伪经纬网的基础上,给出了横向惯导与传统惯导间导航参数的转换关系,推导了横向地理坐标系机械编排,建立了系统误差模型,并以某型船舶为例,通过系统性能的静基座、动基座仿真分析,研究了基于横向地球坐标的惯性导航方法在极区的适用性。仿真分析表明,基于横向地球坐标的惯性导航方法可以克服传统惯导在极区存在的问题,在极点处不存在计算溢出,并可为载体穿越极点时提供高精度的姿态、位置信息,适用于极区。

关 键 词:惯性导航  地球椭球体模型  横向地球坐标  极区

Inertial navigation algorithm for polar region based on transverse terrestrial coordinate
Abstract:Conventional inertial navigation system (INS) mechanization is not applicable in the polar region due to the polar meridians' quickly converging to the poles.To solve this problem,an inertial navigation algorithm with CGCS2000 earth ellipsoid model is proposed based on transverse terrestrial coordinate.Firstly,by constructing the transverse coordinate system and the false graticules,the navigation parameters' transfor-mational relation between transverse INS and conventional INS was presented.Then,the mechanization based on the transverse geographic coordinate system was deduced,and the error model of the system was established.Finally,by taking a certain type of ship as an example,the applicability of the inertial navigation algorithm based on the transverse terrestrial coordinate in polar region was studied by simulating and analyzing the system performances under the conditions of static base and dynamic base respectively.Simulation and analysis results show that the algorithm can overcome the above problem,and there is no calculation overflow at the poles.It can also provide high-precision attitude and position information for carriers passing through the poles.
Keywords:inertial navigation system  earth ellipsoid model  transverse terrestrial coordinate  polar region
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号