摘要
惯性导航系统中敏感器的冗余设计是提高系统任务可靠性的重要方法。文中提出了四冗余惯导系统的配置方案,并对配置方案的可靠性、精度、故障检测及隔离等内容进行了分析论证。
The redudancy design of strapdown inertial system is an important method of improving the system＇s duty reliability. The configuration of the redundancy system using four gyroscopes is presented in this paper . the reliability, accuracy, fault-detection and separation of the configuration is analyzed in detail.
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第3期40-42,45,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
航天科研基金资助项目
