SAE AIR6110 Contiguous Aircraft/System Development Process Example
作者:标准资料网 时间:2024-05-09 14:00:06 浏览:9907
来源:标准资料网
下载地址: 点击此处下载
Product Code:SAE AIR6110
Title:Contiguous Aircraft/System Development Process Example
Issuing Committee: S-18, Aircraft And Sys Dev And Safety Assessment Committee
Scope:This AIR describes, in detail, a contiguous example of the aircraft and systems developmentfor a fictitious aircraft design. In order to present a clear picture, an aircraft function was brokendown into a single system. A function was chosen which had sufficient complexity to allow use ofall the methodologies, yet was simple enough to present a clear picture of the flow through theprocess. This function/system was analyzed using the methods and tools described in the body ofthis ARP document. The interaction of the braking system functions with the aircraft are identifiedwith the criticality identified based on implied aircraft interactions and system availabilities at theaircraft level. This example does not include validation and verification of the aircraft level hazardsand interactions with the braking system. However, the principles used at the braking system levelcan be applied at the higher aircraft level (departing runway). The methodologies applied here arean example of one way to utilize the principles defined in ARP4754A. The basic ARP4754A document contains information which places the information in this appendix in context. This AIR should be used in conjunction with the main body and the other appendices of the ARP4754A. In addition, this example shows the interrelationships with ARP4761.
Title:Contiguous Aircraft/System Development Process Example
Issuing Committee: S-18, Aircraft And Sys Dev And Safety Assessment Committee
Scope:This AIR describes, in detail, a contiguous example of the aircraft and systems developmentfor a fictitious aircraft design. In order to present a clear picture, an aircraft function was brokendown into a single system. A function was chosen which had sufficient complexity to allow use ofall the methodologies, yet was simple enough to present a clear picture of the flow through theprocess. This function/system was analyzed using the methods and tools described in the body ofthis ARP document. The interaction of the braking system functions with the aircraft are identifiedwith the criticality identified based on implied aircraft interactions and system availabilities at theaircraft level. This example does not include validation and verification of the aircraft level hazardsand interactions with the braking system. However, the principles used at the braking system levelcan be applied at the higher aircraft level (departing runway). The methodologies applied here arean example of one way to utilize the principles defined in ARP4754A. The basic ARP4754A document contains information which places the information in this appendix in context. This AIR should be used in conjunction with the main body and the other appendices of the ARP4754A. In addition, this example shows the interrelationships with ARP4761.
下载地址: 点击此处下载