摘要
无人机导航系统设计中,惯导系统的容错能力的提高是需要解决的重点问题之一。在分析余度配置方法和奇偶方程的基础上,给出一种简单易行的惯性器件余度配置方法,并进行了仿真。仿真结果表明,该方法简单易行,有一定的借鉴意义和实用价值。
In the design of UAV navigation system′s,the improved of fault tolerance ability is one of the important problems which needs to be resolved.Based on analyzing remaining degree allocation method and parity equation,give a kind of inertial remaining degree allocation method.Imitation expressed,that method is easily goes and certainly drew lessons from meaning with practical value.
出处
《工业仪表与自动化装置》
2010年第3期92-94,共3页
Industrial Instrumentation & Automation
关键词
惯导系统
容错
余度配置
INS
fault tolerance ability
remaining degree allocation
