对无陀螺捷联惯性制导系统中的数值积分方法的讨论  

Discussion of the Numerical Integration Algorithm Used in the Gyroscope Free Strapdown Inertial Navigation Guidance System

作　　者：赵龙[1] 史震[1] 马澍田[1] 

机构地区：[1]哈尔滨工程大学自动化学院,黑龙江哈尔滨150001

出　　处：《弹箭与制导学报》2001年第2期11-15,共5页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：介绍了无陀螺捷联惯性制导系统的原理和技术 ,并针对无陀螺捷联惯性制导系统中的数值积分问题进行分析和仿真 ,对各种积分方法进行了分析和比较 。The paper introduce the principle and technique of the gyroscope free strapdown inertial navigation guidance system. The numerical integration algorithm about the gyroscope free strapdown inertial navigation guidance system is discussed and simulated, at the same time , several integration algorithm are also analyzed. As a result, some valuable conclusions are obtained.

关 键 词：无陀螺捷联惯导系统 数值积分 导弹制导 数值仿真 

分 类 号：TJ765.2[兵器科学与技术—武器系统与运用工程]