| 发明名称 |
AIRCRAFT SYSTEM VERIFICATION |
| 摘要 |
A verification method for an aircraft system comprises retrieving logical design data associated with the system, and physical design data associated with the system; extracting data from a computer model of the system; converting the retrieved logical and physical design data and the extracted data into a common data format; and performing a difference analysis of the logical and physical design data with the extracted data from the model to identify any non-conformances between the logical design data, the computer model and the physical design data. |
| 申请公布号 |
US2015149124(A1) |
申请公布日期 |
2015.05.28 |
| 申请号 |
US201514605934 |
申请日期 |
2015.01.26 |
| 申请人 |
The Boeing Company |
发明人 |
Hadley Brent L.;Eames Patrick J.;Sciarra Michael P.;Floyd Joseph F.;Williams Charles Mark |
| 分类号 |
G06F17/50 |
主分类号 |
G06F17/50 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A verification method for an aircraft system, the method comprising:
retrieving logical design data associated with the system, and physical design data associated with the system; extracting data from a computer model of the system; converting the retrieved logical and physical design data and the extracted data into a common data format; and performing a difference analysis of the logical and physical design data with the extracted data from the model to identify any non-conformances between the logical design data, the computer model and the physical design data. |
| 地址 |
Chicago IL US |
