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Cockpit management and data system (COMAND), function - GF82.85-P-0003SXJ

MODEL 216.3, 221.0 /1 with CODE (498) Japan version up to Model Year 8 

General 

The COMAND system mainly consists of the following 3 control units:

The control units communicate via different data bus systems and discrete lines with each other.

The COMAND system contains the following functions:

Operation 

The functions of the COMAND controller unit can be used as follows:

The following systems can be centrally operated with the aid of the front central operating unit:

With code (864) Rear entertainment system

Partial functions of the following systems can be operated with the aid of the MFL:

IMPORTANT All button operations on the MFL are initially processed by the instrument cluster. The instrument cluster links the incoming pushbutton operations with the current menu setting in the multifunction display (A1p13) and, where applicable, it then transmits a corresponding message via the central CAN to the COMAND controller unit.

COMAND data bus systems 

The digital components of the COMAND system are networked via a data bus system, over which control commands and useful information are transmitted between the individual system components.

The individual component operate with various data formats and they have different request in terms of transmission rate and reliability. Thus, different data bus systems are installed.

IMPORTANT The COMAND controller unit represents the interface between the Media Oriented System Transport (MOST) and the central CAN, as well as between the MOST and the telematics CAN.

The following data bus systems are part of the COMAND system:

VCS 

The voice control enables the user to be relieved during a journey and provide him/her with access to a series of functions, without diverting attention from the traffic situation. Furthermore, this function should enable the driver to intuitively operate the system. The VCS [SBS] is controlled via the software integrated into the COMAND controller unit. Pressing the VCS [SBS] on button (S111s4) on the MFL activates the voice control, while pressing the "Back" and VCS [SBS] off button (S110s4) deactivates it. An acoustic signal is emitted after activation has taken place.

The following functions can be controlled via the VCS:

Help function of the VCS [SBS] (phonetic spelling) 

In addition to the number and name, the phonetic spelling of the name is also stored in the telephone book of the portable CTEL (A34/6). If the portable CTEL phonebook contents are transferred to the COMAND controller unit, then all the phonebook entries are available immediately, also for the voice control system.

  Cockpit Management and Data System (COMAND) Volume/tone setting   GF82.85-P-0003-06SX 
  Cockpit Management and Data System (COMAND) Switch on/off behavior   GF82.85-P-0003-07SX 
  Cockpit management and data system (COMAND), networking of components   GF82.85-P-0003-10SXJ 
  Audio mode, function Radio; CD; audio DVD; music register; VICS GF82.85-P-2030SXJ 
  Communications, function Telephone; e-mail; Bluetooth; Internet GF82.85-P-2016SXJ 
  Video mode, function Video DVD; TV; backup camera GF82.85-P-2040SXJ 
  Navigation mode, function   GF82.85-P-2012SXJ