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Cockpit Management and Data system (COMAND), function - GF82.85-P-0003R

MODELS 203.0 /2 /7 up to 23.4.04 with CODE (352a) COMAND operating and display system with CODE (491) U.S. version 

Fig 1: Cockpit Management And Data System (COMAND) Function Diagram - Models 203.0 /2 /7 Up To 23.4.04 With Code (352A) And (491)
G04735676

Block diagram, overall system 

Illustrated with following equipment: 

Cockpit management and data system (COMAND), function 

The COMAND operating, display and control unit (A40/3) is the central component in the COMAND system. It has a video-capable Liquid Crystal Display (LCD) color display to output information such as operating menus and map data for navigation. It is operated by means of fixed function keys and two rotary controls as well as menu-guided in the display. Several functions can also be activated with the aid of the buttons on the multifunction steering wheel (MFL). It should be noted that all button operations on the multifunction steering wheel (MFL) are first processed by the instrument cluster (A1). The instrument cluster (A1) combines the incoming button signals with the current menu setting on the multifunction display (A1p13) and sends an appropriate Controller Area Network (databus/CAN bus) (CAN) message to the COMAND operating, display and control unit (A40/3) if necessary.

The vehicle can also be equipped optionally with an infrared remote control for issuing commands from the rear of the passenger compartment as well as a voice control system (VCS) (code 813) for telephone functions and several audio functions, both of which serve to further enhance operating convenience.

Bus system (COMAND) 

The digital components in the COMAND operating, display and control unit (A40/3) are networked with each other through a bus system. The bus system is used to transmit data (control commands and useful information) between the various system components.

Because some of the individual components work with different data formats or require different data transfer rates and security levels, the following different bus systems have been installed:

The digital data bus (D2B) is used for data exchange between the sound amplifier (A2/13) (with code 810), the CD player with changer (in glove compartment) (A2/6) (with code 819a), the telephone system and, if installed, the voice control system (VCS) (with code 813). Both control data as well as the actual audio signals are transmitted.

The CAN-B is used for data exchange with the instrument cluster (A1). In this way, the instrument cluster (A1) receives, from the COMAND operating, display and control unit (A40/3), the audio, telephone and navigation data for the multifunction display (A1p13) in the instrument cluster (A1) as well as the time of day.

  Cockpit Management and Data System (COMAND), driver information Displays in the instrument cluster GF82.85-P-0003-03R 
  Radio mode, function   GF82.60-P-2001R
  CD-player mode, function   GF82.60-P-2002R
  Volume/tone adjustments, function   GF82.60-P-2003R
  Navigation mode, function   GF82.85-P-2012R 
  Starguide, function   GF82.85-P-2014A 
  Information service, function   GF82.85-P-3016A 
  Data transmission for Starguide, function   GF82.85-P-3017A 
  Switch on/off behavior, function   GF82.85-P-2006R 
  Telephone mode, function   GF82.85-P-2007R 
  Cassette mode, function   GF82.85-P-2010R 
  Data transfer between COMAND and instrument cluster, function   GF82.85-P-3008R