TY - GEN
T1 - Research on Airworthiness Qualification Test Technology of Radiation Emission in Civil Aircraft Flight Control Electronic System
AU - Kuan, Lu
AU - Aijun, Li
AU - Tianbo, Wang
AU - Linxiao, Li
AU - Jianyuan, Wang
N1 - Publisher Copyright:
© 2022, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
PY - 2022
Y1 - 2022
N2 - It is the first time that domestic civil large aircraft has been developed, which lacks the technical experience of airborne system-level airworthiness qualification, and the research of radiation emission at home and abroad is mainly based on simulation evaluation, while the simulation results are used only as a reference in the airworthiness qualification process and cannot be used as evidence of conformity. And there is little airworthiness test experience on complex system-level. In this paper, taking civil aircraft flight control electronic system as an example, through the demonstration of the airworthiness requirement, the description of the complexity of civil aircraft flight control electronic system, demonstrate the airworthiness qualification test and optimization process, providing experience for the airworthiness qualification of civil aircraft complex system. The results show that the radiation emission of flight control electronic system is greatly affected by the system environment, and it is necessary to consider the test setup layout and show the system compliance to the DO-160G requirements.
AB - It is the first time that domestic civil large aircraft has been developed, which lacks the technical experience of airborne system-level airworthiness qualification, and the research of radiation emission at home and abroad is mainly based on simulation evaluation, while the simulation results are used only as a reference in the airworthiness qualification process and cannot be used as evidence of conformity. And there is little airworthiness test experience on complex system-level. In this paper, taking civil aircraft flight control electronic system as an example, through the demonstration of the airworthiness requirement, the description of the complexity of civil aircraft flight control electronic system, demonstrate the airworthiness qualification test and optimization process, providing experience for the airworthiness qualification of civil aircraft complex system. The results show that the radiation emission of flight control electronic system is greatly affected by the system environment, and it is necessary to consider the test setup layout and show the system compliance to the DO-160G requirements.
KW - Airworthiness
KW - Flight control electronic
KW - Qualification test
KW - Radiated emissions
UR - http://www.scopus.com/inward/record.url?scp=85119890761&partnerID=8YFLogxK
U2 - 10.1007/978-981-16-7423-5_94
DO - 10.1007/978-981-16-7423-5_94
M3 - 会议稿件
AN - SCOPUS:85119890761
SN - 9789811674228
T3 - Lecture Notes in Electrical Engineering
SP - 951
EP - 962
BT - Proceedings of the 5th China Aeronautical Science and Technology Conference
PB - Springer Science and Business Media Deutschland GmbH
T2 - 5th China Aviation Science and Technology Conference, 2021
Y2 - 1 January 2021
ER -