TY - GEN
T1 - Launch vehicle fault injection and fault diagnosis based on mil-std-1553b data bus
AU - Chen, Juan
AU - Xie, Shilu
AU - Li, Jia
AU - Guo, Botao
AU - Wang, Deyi
N1 - Publisher Copyright:
© ESREL2020-PSAM15 Organizers. Published by Research Publishing, Singapore.
PY - 2020
Y1 - 2020
N2 - Fault diagnosis is critical to the operation of the launch vehicle, not only to avoid casualties and equipment losses, but also to save on operating costs. Considering the numerous launch vehicle systems, complex functions and various faults, this paper studies a fault diagnosis method based on MIL-STD-1553B (hereinafter referred to as 1553B) data bus, which can diagnose and predict system failure in real time and give decision on successful launch probability. By using the fault tree, the fault of the launch vehicle is detected and located, the failure chain is determined. Generally, it is difficult to obtain sufficient fault data in the ground test, which limits the fault diagnosis research. In order to get more failure data, a fault injection method based on 1553B bus is designed in this paper. In the launch vehicle fault diagnosis and injection system, the fault diagnosis system acts as a bus monitor (BM), and the fault injection system acts as a remote terminal (RT). They are connected to the 1553B bus, which connects the subsystem of the launch vehicle, and connects to the launch control platform outside the vehicle through the bus coupler. The simulations provided impetus for practical tests and the experimental test show expected results.
AB - Fault diagnosis is critical to the operation of the launch vehicle, not only to avoid casualties and equipment losses, but also to save on operating costs. Considering the numerous launch vehicle systems, complex functions and various faults, this paper studies a fault diagnosis method based on MIL-STD-1553B (hereinafter referred to as 1553B) data bus, which can diagnose and predict system failure in real time and give decision on successful launch probability. By using the fault tree, the fault of the launch vehicle is detected and located, the failure chain is determined. Generally, it is difficult to obtain sufficient fault data in the ground test, which limits the fault diagnosis research. In order to get more failure data, a fault injection method based on 1553B bus is designed in this paper. In the launch vehicle fault diagnosis and injection system, the fault diagnosis system acts as a bus monitor (BM), and the fault injection system acts as a remote terminal (RT). They are connected to the 1553B bus, which connects the subsystem of the launch vehicle, and connects to the launch control platform outside the vehicle through the bus coupler. The simulations provided impetus for practical tests and the experimental test show expected results.
KW - Failure chain
KW - Fault diagnosis
KW - Fault injection
KW - Fault tree
KW - Launch vehicle
KW - MIL-STD-1553B data bus
UR - https://www.scopus.com/pages/publications/85107288805
U2 - 10.3850/978-981-14-8593-0_5153-cd
DO - 10.3850/978-981-14-8593-0_5153-cd
M3 - 会议稿件
AN - SCOPUS:85107288805
SN - 9789811485930
T3 - Proceedings of the 30th European Safety and Reliability Conference and the 15th Probabilistic Safety Assessment and Management Conference
SP - 3621
EP - 3628
BT - Proceedings of the 30th European Safety and Reliability Conference and the 15th Probabilistic Safety Assessment and Management Conference
A2 - Baraldi, Piero
A2 - Di Maio, Francesco
A2 - Zio, Enrico
PB - Research Publishing, Singapore
T2 - 30th European Safety and Reliability Conference, ESREL 2020 and 15th Probabilistic Safety Assessment and Management Conference, PSAM15 2020
Y2 - 1 November 2020 through 5 November 2020
ER -