#Ace for flight control system pdf
#Ace for flight control system full
#Ace for flight control system software

125000004122 cyclic group Chemical group 0.000 description 1.

230000001276 controlling effect Effects 0.000 description 1.

206010038192 Red man syndrome Diseases 0.000 description 1.

238000006011 modification reaction Methods 0.000 description 2.

230000005540 biological transmission Effects 0.000 description 2.

238000006243 chemical reaction Methods 0.000 description 3.

Publication of US20070083301A1 publication Critical patent/US20070083301A1/en Application granted granted Critical Publication of US7421320B2 publication Critical patent/US7421320B2/en Status Active legal-status Critical Current Adjusted expiration legal-status Critical Links Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.) Filing date Publication date Application filed by Boeing Co filed Critical Boeing Co Priority to US11/245,729 priority Critical patent/US7421320B2/en Assigned to BOEING COMPANY, THE reassignment BOEING COMPANY, THE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Original Assignee Boeing Co Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.) ( en Inventor Ying Yeh Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.) Granted Application number US11/245,729 Other versions US7421320B2

#Ace for flight control system pdf

Google Patents Methods and apparatus for implementing mid-value selection functions for dual dissimlar processing modulesДownload PDF Info Publication number US20070083301A1 US20070083301A1 US11/245,729 US24572905A US2007083301A1 US 20070083301 A1 US20070083301 A1 US 20070083301A1 US 24572905 A US24572905 A US 24572905A US 2007083301 A1 US2007083301 A1 US 2007083301A1 Authority US United States Prior art keywords pfc control signal data fresh data fresh Prior art date Legal status (The legal status is an assumption and is not a legal conclusion.

Google Patents US20070083301A1 - Methods and apparatus for implementing mid-value selection functions for dual dissimlar processing modules

The entire system can be contacted via an ARINC 600 plug on its back.US20070083301A1 - Methods and apparatus for implementing mid-value selection functions for dual dissimlar processing modules The screen definition of each display can be adjusted individually. In addition to that, the Display System includes four CAN bus interfaces (1Mb/s similar to the ones of the A380) and three optical interfaces (glass fiber) for a data transfer of up to 3.1 Gb/s.

#Ace for flight control system full

The communication between the six Display Systems that are integrated into the cockpit utilises the integrated AFDX Modules (100Mb/s full duplex). The work share of Diehl Aerospace consists of a metal housing with integrated ventilators for the cooling in the case of an emergency, of a Power Supply-I/O Board including an attached AFDX Module and a graphics processor board.

#Ace for flight control system software

The Display System allows the presentation of flight and navigation parameters as well as the communication between the crew and the various software applications.

Diehl Aerospace in cooperation with Thales provides Multifunction Displays for all Airbus aircraft types and develops the Display System for the A350 XWB.