كيف استخدم ال:icon_arroFMC في الطائرة

هذه مجموعة من مقاطع الفيديو

للطائرة التشبيهية لطريقة أستخدام

FMC


وأن شاء الله من خلال هذه المقاطع راح توضح لك الفكرة

نوع الطائرة 747-400

أف أم سي القسم الاول

اف ام سي القسم الثاني

اف ام سي القسم الثالث

المشاركة الأصلية كتبت بواسطة شهاب الجزيرة (المشاركة 186764) هذه مجموعة من مقاطع الفيديو للطائرة التشبيهية لطريقة أستخدام FMC وأن شاء الله من خلال هذه المقاطع راح توضح لك الفكرة نوع الطائرة 747-400 أف أم سي القسم الاول اف ام سي القسم الثاني اف ام سي القسم الثالث

The flight management computing system shares data with the these systems or components:

The FMCS uses the data from the airplane systems to do these functions:

The FMCS has these components:

Also, the mode control panel (MCP) has an interface with the FMCS, but is not an FMCS component.

Each FMCF has these two software partitions:

The FMF partition supplies these functions:

The navigation function partition supplies these functions:

The FMCFs use performance and navigation data bases and sensor inputs to calculate guidance commands. When the flight crew uses the MCP to select the LNAV and VNAV modes, the FMCF sends this data:

The automatic dependent surveillance function (ADSF) is a sub-function of the FMCF. The purpose of the ADSF is to let air traffic control (ATC) monitor the airplane in the air.
ATC sends automatic dependent surveillance (ADS) requests from the ground to the airplane. The ADSF in the airplane sends airplane position, heading, airspeed, and other data to the ground. ATC uses this data to manage air traffic. The ADSF is automatic and does not require flight crew action.

There are three CDUs in the flight deck. The CDUs are the primary control and display interface unit for the FMCF. The flight crew uses the left and right CDUs to enter flight plan data and interface with the FMCF and other systems. If the left or right CDU fails, the center CDU is the backup.
All CDUs can select a maintenance page format on a multifunction display (MFD) in the primary display system (PDS).
All CDUs can control the satellite communication (SATCOM) system.
The center CDU is the interface for the passenger address/cabin interphone (PA/CI) controller.
The CDU supplies these functions when the FMCFs fail:

The FMC selector is on the first officer display switching panel. It determines the active FMCF.
The FMC selector and ISSP switches supply analog inputs to the overhead panel ARINC 629 system (OPAS). The OPAS changes these inputs and sends them to the AIMS cabinet on the systems ARINC 629 buses.
The NAV ISSP switch determines the source of navigation display data.