A Simulation based Intelligent Analysis Framework of Aircraft Reliability, Resilience and Vulnerability

被引:1
作者
Yao, Qi [1 ]
Zeng, Fuping [1 ]
Zhang, Yizhuo [1 ]
Yang, Minghao [1 ]
Duan, Zhiyu [1 ]
Yang, Shunkun [1 ]
机构
[1] Beihang Univ, Sch Reliabil & Syst Engn, Beijing, Peoples R China
来源
2021 IEEE 21ST INTERNATIONAL CONFERENCE ON SOFTWARE QUALITY, RELIABILITY AND SECURITY (QRS 2021) | 2021年
基金
中国国家自然科学基金;
关键词
737; MAX; Maneuvering Characteristics Augmentation System (MCAS); reliability; resilience; vulnerability; multimodal optimization; PERFORMANCE ASSESSMENT; CIVIL AIRCRAFT; MODEL; CONVERGENCE;
D O I
10.1109/QRS54544.2021.00046
中图分类号
TP31 [计算机软件];
学科分类号
081202 ; 0835 ;
摘要
The flight reliability has been receiving considerable attention. However, the ability of the aircraft recovers to normal flight state from a perturbation were not considered under most circumstances. In this study, a simulation based intelligent analysis framework is proposed to identify the reliability, resilience and vulnerability states of Boeing 737 MAX aircraft disturbed by Maneuvering Characteristics Augmentation System (MCAS) system abnormal activation during the flight. Multiswarm particle swarm optimization (multiswarm PSO) algorithm based test cases generation strategy, aircraft failure behavior model which reflects aerodynamics of the aircraft after the horizontal stabilizer deflection caused by MCAS abnormal activation, JSBSim and FlightGear based co-simulation with aerodynamic and visual characteristics and neural network based flight states identification method constitute the proposed framework. Study results show that the proposed method can cover the margin of resilience and vulnerability quickly and the classification model can identify aircraft flight reliability, resilience and vulnerability states corresponding to different inputs accurately. The proposed framework can be used to validate the flight reliability and system resilience in a more efficient way.
引用
收藏
页码:347 / 356
页数:10
相关论文
共 39 条
[31]   Analysis and Simulation of Flight Effects on an Airborne Magnetic Gradient Tensor Measurement System [J].
Sui, Yangyi ;
Kang, Pan ;
Cheng, Defu ;
Lin, Jun .
IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, 2015, 64 (10) :2657-2665
[32]   Investigation of pitch damping derivatives for the Standard Dynamic Model at high angles of attack using neural network [J].
Tatar, Massoud ;
Masdari, Mehran .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 92 :685-695
[33]  
Wang L., AEROSP SCI TECHNOL
[34]   Active fault-tolerant control strategy of large civil aircraft under elevator failures [J].
Wang Xingjian ;
Wang Shaoping ;
Yang Zhongwei ;
Zhang Chao .
CHINESE JOURNAL OF AERONAUTICS, 2015, 28 (06) :1658-1666
[35]   An ensemble radius basis function network based on dynamic time warping for real-time monitoring of supersonic inlet flow patterns [J].
Wu, Huan ;
Zhao, Yong-Ping ;
Yang, Tian-Lin ;
Tan, Hui-Jun .
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 111
[36]   An on-line deep learning framework for low-thrust trajectory optimisation * [J].
Xie, Ruida ;
Dempster, Andrew G. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 118 (118)
[37]   Propeller design to improve flight dynamics features and performance for coaxial compound helicopters [J].
Yuan, Ye ;
Chen, Renliang ;
Thomson, Douglas .
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 106
[38]   A cluster based PSO with leader updating mechanism and ring-topology for multimodal multi-objective optimization [J].
Zhang, Weizheng ;
Li, Guoqing ;
Zhang, Weiwei ;
Liang, Jing ;
Yen, Gary G. .
SWARM AND EVOLUTIONARY COMPUTATION, 2019, 50
[39]   Reliable flight performance assessment of multirotor based on interacting multiple model particle filter and health degree [J].
Zhao, Zhiyao ;
Yao, Peng ;
Wang, Xiaoyi ;
Xu, Jiping ;
Wang, Li ;
Yu, Jiabin .
CHINESE JOURNAL OF AERONAUTICS, 2019, 32 (02) :444-453