Anomaly Detection Method for Rocket Engines Based on Convex Optimized Information Fusion

Author:

Sun Hao1,Cheng Yuehua1ORCID,Jiang Bin1ORCID,Lu Feng2ORCID,Wang Na1

Affiliation:

1. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China

2. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Abstract

The power system, as a core component of a launch vehicle, has a crucial impact on the reliability and safety of a rocket launch. Due to the limited measurement information inside the engine, it is often challenging to realize fast and accurate anomaly detection. For this reason, this paper introduces the rocket flight state data to expand the information source for anomaly detection. However, engine measurement and rocket flight state information have different data distribution characteristics. To find the optimal data fusion scheme for anomaly detection, a data set information fusion algorithm based on convex optimization is proposed, which solves the optimal fusion parameter using the convex quadratic programming problem and then adopts the adaptive CUSUM algorithm to realize the fast and accurate anomaly detection of engine faults. Numerical simulation tests show that the algorithm proposed in this paper has a higher detection accuracy and lower detection time than the traditional algorithm.

Funder

National Key Research and Development Program of China

National Natural Science Foundation Integration Project

Publisher

MDPI AG

Reference36 articles.

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2. Huang, P., Yu, H., and Wang, T. (2022). A Study Using Optimized LSSVR for Real-Time Fault Detection of Liquid Rocket Engine. Processe, 10.

3. Deep neural network approach for fault detection and diagnosis during startup transient of liquid-propellant rocket engine;Park;Acta Astronaut.,2020

4. A supervised framework for recognition of liquid rocket engine health state under steady-state process without fault samples;Lv;IEEE Trans. Instrum. Meas.,2021

5. Oreilly, D. (1993). System for Anomaly and Failure Detection (SAFD) System Development (No. NAS 1.26: 193907), NASA.

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