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Consideration and validation of flight control requirements under all engine failure conditions for MEA

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Consideration and validation of flight control requirements under all engine failure conditions for MEA

Content Provider	IET Digital Library
Author	Li, Xiyu Xu, Shuhan Bai, Zhiqiang
Abstract	Since the lower carbon emission and lower direct operating cost, MEA has drawn great attention worldwide. Considering and validating the flight control requirements under all engine failure conditions for MEA is the minimum design requirement, which is widely associated with aircraft characteristics, controllability and manoeuvrability, and system specialities such as electrical system, power plant system, hydraulic system, and avionics. Therefore, taking this topic as an example to illustrate a requirement validation process will be great interest to the aircraft design and integration, where the correctness and completeness of the requirements would be satisfied, the method and evidences of validation would be proposed, the requirement assumption validation and management should be presented, and scenario analysis and typical timeline analysis would be analysed. This paper presents the above processes from configuration, requirement definition and validation, to scenario analysis in compliance with SAE 4754A, which will be a fundamental process to the further verification and integration tasks.
Starting Page	392
Ending Page	398
Page Count	7
Volume Number	2018
e-ISSN	20513305
Issue Number	Issue 13, Jan (2018)
Alternate Webpage(s)	https://digital-library.theiet.org/content/journals/joe/2018/13
Alternate Webpage(s)	https://digital-library.theiet.org/content/journals/10.1049/joe.2018.0062
Journal	The Journal of Engineering
Publisher	The Institution of Engineering and Technology
Publisher Date	2018-02-02
Access Restriction	Open
Rights License	Creative Commons Attribution-No Derivs License (http://creativecommons.org/licenses/by-nd/3.0/)
Subject Keyword	Aerospace Control Aerospace Engines Aerospace Industry Aerospace Safety Aircraft Characteristic Aircraft Control Aircraft Design Aircraft Integration Tasks Avionics Controllability Design Engineering Electrical System Engine Failure Condition Engines Failure Analysis Flight Control Requirements Validation Health And Safety Aspects Hydraulic System Low Carbon Emission Maintenance And Reliability Manoeuvrability MEA Operating Cost Power Plant System SAE 4754A Timeline Analysis
Content Type	Text
Resource Type	Article

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