Predictive Health Status Assessment of a Launch Vehicle Engine in an Ascending Flight Based on Vibration Signals
Author:
Affiliation:
1. School of Integrated Circuits and Electronics, Beijing Institute of Technology, Beijing, China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Aerospace Engineering
Link
http://xplorestaging.ieee.org/ielx7/7/10353051/10184911.pdf?arnumber=10184911
Reference29 articles.
1. Vibration characteristics of airborne multiple launch rocket systems;Zhang;J. Vib. Eng.,2013
2. Fault detection and diagnosis algorithms for transient state of an open-cycle liquid rocket engine using nonlinear Kalman filter methods
3. An approach for on-line extraction of fuzzy rules using a self-organising fuzzy neural network
4. A Self-Evolving Fuzzy System Which Learns Dynamic Threshold Parameter by Itself
5. A Metacognitive Neuro-Fuzzy Inference System (McFIS) for Sequential Classification Problems
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