Safety system: self-test fault

The BYTEFLIGHT bus system has a star-shaped structure. The individual satellites (= control units with/without sensors) are interconnected across a star coupler by means of fibre-optic cables. The star coupler in the BYTEFLIGHT bus system is the Safety and Information Module. There is a transmission and a reception module (transmitter and receiver) as a unit in each satellite for connecting to the BYTEFLIGHT bus. The unit has an integrated transmit and receive diode.

Main functions

Fault code memory entries

The procedure for the following fault code memory entries is shown below:

  1. Self test: too few messages
  2. Self test: data fault in message
  3. Self test: communication fault
    According to a fixed and known pattern, messages are sent during a communication test (self test). A control unit transmits a message with known content and this is received and tested by several control units. During this test, faults 1 to 3 can occur in the receiving control units.

Two cases are distinguished:

Important: The following tables specify the door satellites STVL and STVR. However, these two door satellites are only fitted in the USA version!

The following Table 1 shows which control units generate a fault code memory entry if a transmitting control unit does not send a certain message. The first vertical column contains the transmitting control units (TCU); the first horizontal line contains the receiving control units (RCU).

Table 1:

 

RCU

SBSL

SBSR

SIM

STVL

STVR

TCU

 

 

 

 

 

 

SIM

 

X

X

 

X

X

SBSL

 

 

X

X

X

X

SBSR

 

X

 

X

X

X

STVL

 

X

 

 

 

X

STVR

 

X

 

 

X

 

Table 2:

 

RCU

SBSL

SBSR

SIM

STVL

STVR

TCU = ?

 

X

X

X

X

SIM

Safety and information module

SBSL

Satellite, B-pillar left

SBSR

Satellite, B-pillar right

STVL

Door satellite, front left

STVR

Door satellite, front right

Service functions

Notes on safety

All work on the airbags must be carried out with the battery disconnected!

Connect and disconnect all BYTEFLIGHT control units, sensors and generators only with the battery disconnected!

If a fibre-optic cable on the BYTEFLIGHT bus has to be repaired, it must be borne in mind that there may only be one join between the Safety and Information Module and a satellite. For this reason, no repairs may be performed on the fibre-optic cable between the Safety and Information Module and the door satellites, as there is already a join with the door connector. In the case of a defect, the fibre-optic cable must be replaced!