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

惯性平台误差标定仿真数据源建模研究
引用本文:连丁磊,夏刚,王汀.惯性平台误差标定仿真数据源建模研究[J].导航与控制,2011(4):1-5.
作者姓名:连丁磊  夏刚  王汀
作者单位:北京航天控制仪器研究所;北京航天控制仪器研究所;北京航天控制仪器研究所
摘    要:为满足平台导航方式自标定算法对仿真数据源的需求,归纳总结了标定算法对仿真数据源的要求,提出了用于产生标定仿真数据的平台运动学模型.该模型在反映误差作用的同时回避了平台复杂控制系统和动力学特性,采用运动学微分方程描述台体在指令角速度激励下相对惯性空间的运动,通过代数方程描述加速度计的输出和框架角输出.在典型轨迹下,对仿真...

关 键 词:惯性平台  自标定算法  仿真数据源  标定仿真  运动学模型

On the Simulation Data Source of PINS Self-calibration
LIAN Ding-lei,XIA Gang and WANG Ting.On the Simulation Data Source of PINS Self-calibration[J].Navigation and Control,2011(4):1-5.
Authors:LIAN Ding-lei  XIA Gang and WANG Ting
Institution:Beijing Institute of Aerospace Control Device;Beijing Institute of Aerospace Control Device;Beijing Institute of Aerospace Control Device
Abstract:The Simulation Data Source of Platform Inertial Navigation System(PINS) seif-calibration is investigated. By thorough analysis of the Simulation requirements,this paper concludes and summarizes the demand of the simulation data source,and gives the kinetic model which used to produce the data of calibration and simulation. This model not only reflects the error but also avoids the character of the complex control and dynamics,describes the platform case movement to inertial coordinate which is got by solving the differential equation numerically,and gives the output of the accelerometer and the gimbals tangle by solving the algebraic equation. At the typical track of the platform movement, this paper exams the result compared with the academic data,and it indicates that the accuracy on the basis of this simulation which is designed according to the model meets the demand of the self-calibration algorithm.
Keywords:PINS  self-calibration algorithm  simulation data source  calibration and simulation  kinetic model
点击此处可从《导航与控制》浏览原始摘要信息
点击此处可从《导航与控制》下载免费的PDF全文
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