摘要
研究了解析冗余及容错技术在某型飞机综合导航系统中的应用 ,并就此相应的数学模型和故障检测方法进行了讨论 。
The application on analytical redundancy and fault tolerate technique for a certain type of integrated navigation system is studied in this paper, and its corresponding mathematic model and fault test method is discussed, the conclusion has good value for improving the veracity and reliability of other navigation system and information fusion.
出处
《弹箭与制导学报》
CSCD
北大核心
2002年第4期25-27,31,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
导航系统
综合导航参数
解析冗余
故障诊断
容错控制
飞机
integrated navigation system
analytical redundancy
fault diagnosis
fault tolerate control
