飞行器惯性导航误差仿真平台设计  

Design of Aircraft Inertial Navigation Error Simulation Platform

作　　者：郭庆叶[1] 柳明[1] 

机构地区：[1]滨州学院飞行学院,山东滨州256603

出　　处：《滨州学院学报》2013年第6期38-43,共6页Journal of Binzhou University

基　　金：山东省高等学校科技计划项目(J13LN74);滨州学院"青年人才创新工程"科研基金(BZXYQNLG200810)

摘　　要：为直观反映惯性器件及平台初始误差对导航精度的影响,在给出仿真平台的数学模型的基础上设计开发了惯性导航误差仿真平台.仿真平台采用Matcom实现Matlab与VC++之间的混合编程,结果表明,该方法提高了软件的开发效率.该仿真平台简单易操作,可直观反映惯性器件及平台初始误差对导航精度的影响,对提高惯导系统的导航精度具有指导意义.In order to reflect the impact directly, the error simulation platform of INS based on the mathematical model of the platform is designed. In order to improve the software development efficiency, the simulation platform is decided to realize mixed programming by Matcom. The results show that the mixed programming shortens the software development period. The simulation platform is easy to operate and reflect the impact directly. It is significance to improve the accuracy of navigation.

关 键 词：惯性导航 仿真平台 混合编程 MATCOM 

分 类 号：TN911.1[电子电信—通信与信息系统]