摘要
针对泵压式供应系统液体火箭发动机的健康监控问题，提出了故障检测与诊断的基本框架，并讨论了基于发动机系统非线性数学模型、推广的卡尔曼滤波的故障检测方法和基于低阶线性模型的故障诊断方法。
For monitoring conditions of a liquid rocket engine with turbo-pump system, an outline of fault detection and diagnosis is presented in this paper. The fault detection method with extended Kalman filter based on nonlinear mathematical models and the diagnosis method based on lower-order linear models are also discussed.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1994年第5期1-8,共8页
Journal of Propulsion Technology
基金
国家自然科学基金
关键词
液体推进剂
火箭发动机
故障检测
数学模型
Liquid propellant rocket engine, Fault detection, Fault diagnosis,Mathematical moldel, Dynamic response, Kalman filtering
