Commission Delegated Regulation (EU) 2017/79 of 12 September 2016 establishing de... (32017R0079)
Commission Delegated Regulation (EU) 2017/79 of 12 September 2016 establishing de... (32017R0079)
COMMISSION DELEGATED REGULATION (EU) 2017/79
of 12 September 2016
establishing detailed technical requirements and test procedures for the EC type-approval of motor vehicles with respect to their 112-based eCall in-vehicles systems, of 112-based eCall in-vehicle separate technical units and components and supplementing and amending Regulation (EU) 2015/758 of the European Parliament and of the Council with regard to the exemptions and applicable standards
(Text with EEA relevance)
Article 1
Subject matter
Article 2
Classes of vehicles exempted from the requirement to be equipped with a 112-based eCall in-vehicle system
Article 3
Multi-stage approval of special purpose vehicles
Article 4
Definitions
Article 5
Requirements and test procedures for EC type-approval of motor vehicles with regard to the installation of 112-based eCall in-vehicle systems
Article 6
Requirements and test procedures for EC type-approval of 112-based eCall in-vehicle system components
Article 7
Requirements and test procedures for EC type-approval of 112-based eCall in-vehicle STUs
Article 8
Obligations of the Member States
Article 9
Amendments to Regulation (EU) 2015/758
Article 10
Entry into force and application
TABLE OF CONTENTS
ANNEX I
Technical requirements and procedures for testing the resistance of eCall in-vehicle systems to severe crashes (high-severity deceleration test)
1. Requirements
1.1. Performance requirements
2. Test procedure
2.1. Purpose of the high-severity deceleration test procedure
2.3. Deceleration/acceleration procedure
2.3.7. Description of the test pulse
Figure
Minimum and maximum curve of the test pulse (pulse corridor)
|
Point |
Time (ms) |
Acceleration/Deceleration (g) |
|
A |
10 |
0 |
|
B |
34 |
65 |
|
C |
38 |
65 |
|
D |
46 |
0 |
|
E |
0 |
16 |
|
F |
25 |
77 |
|
G |
47 |
77 |
|
H |
60 |
0 |
2.4. Verification procedure
2.5. Positioning test procedure
2.6. Antenna test procedure
2.7. Connection procedures
2.7.1. Simulated Mobile Network Procedure
2.7.2. Public Mobile Network Procedure
2.7.3. Wired Transmission Procedure
2.8. Verification procedures for components
2.8.2. Control module including its connectors and wire harness as described in point 2.2.4 of this Annex.
2.8.3. Mobile network antenna including its connectors and wire harness as described in point 2.2.4 of this Annex
2.8.4. Power supply (if not part of the control module) including its connectors and wire harness as described in point 2.2.4 of this Annex
ANNEX II
Full-scale impact test assessment
1. Requirements
1.1. Performance requirements
2. Test procedure
2.1. Purpose of the full-scale impact test procedure
2.3. Impact test procedure
2.4. Verification procedure
2.5. Positioning test procedure
2.6. Antenna test procedure
2.7. Connection procedures
ANNEX III
Crash resistance of audio equipment
1. Requirements
1.1. Performance requirements
2. Test procedure
2.1. Purpose of the audio equipment crash resistance test procedure
2.3. Overview of test procedure
2.4. Arrangement of testers
2.5. Test setup
2.6. Test call
2.6.2. Exchange of test messages
2.6.2.1. Receive direction
2.6.2.2. Send direction
2.7. Connection procedures
Appendix
Test sentences
3. Test sentence pairs
3.1. Dutch
3.2. English
3.3. Finnish
3.4. French
3.5. German
3.6. Italian
3.7. Polish
3.8. Spanish
ANNEX IV
Co-existence of third party services (TPS) with the 112-based eCall in-vehicle systems
1. Requirements
1.2. Performance requirements
1.3. Documentation requirements
2. Test procedure
2.1. Purpose of the TPS co-existence test procedure
2.5. Connection procedures
ANNEX V
Automatic triggering mechanism
1. Requirements
1.2. Documentation requirements
ANNEX VI
Technical requirements for compatibility of eCall in-vehicle systems with the positioning services provided by the Galileo and the EGNOS systems
1. Requirements
1.1. Compatibility requirements
1.2. Performance requirements
2. Test methods
2.1. Test conditions
|
Equipment name |
Required technical characteristics of test equipment |
|||||||
|
Scale range |
Scale accuracy |
|||||||
|
Global navigation satellite system simulator of Galileo and GPS signals |
Number of simulated signals: at least 12 |
Mean square deviation of random accuracy component of pseudo-range to Galileo and GPS satellites not more than:
|
||||||
|
Digital stopwatch |
Maximum count volume: 9 hours 59 minutes 59,99 seconds |
Daily variation at 25 (± 5) °С not more than 1,0 seconds. Time discreteness 0,01 seconds. |
||||||
|
Vector network analyser |
Frequency range: 300 kHz .. 4 000 kHz Dynamic range: (minus 85 .. 40) dB |
Accuracy F = ± 1·10– 6 kHz Accuracy D = (0,1 .. 0,5) dB |
||||||
|
Low-noise amplifier |
Frequency range: 1 200 .. 1 700 MHz Noise coefficient: not more 2,0 dB Amplifier gain coefficient: 24 dB |
|
||||||
|
Attenuator 1 |
Dynamic range: (0 .. 11) dB |
Accuracy ± 0,5 dB |
||||||
|
Attenuator 2 |
Dynamic range: (0 .. 110) dB |
Accuracy ± 0,5 dB |
||||||
|
Power source |
Range of direct current voltage setting: from 0,1 to 30 volts |
Accuracy V = ± 3 % |
||||||
|
Current intensity of output voltage: at least 3 amperes |
Accuracy A = ± 1 % |
|||||||
|
Note: it is allowed to apply other similar types of equipment providing determination of characteristics with the required accuracy. |
||||||||
Figure 1
Open sky definition
|
Zone |
Elevation range (degrees) |
Azimuth range (degrees) |
|
A |
0 – 5 |
0 – 360 |
|
Background |
Area out of Zone A |
|
|
|
0 dB |
|
A |
– 100 dB or signal is switched off |
2.2. Test procedures
2.2.1. NMEA-0183 messages output test.
Figure 2
Diagram of test stand
|
Simulated parameter |
Value |
||||||
|
Test duration, hh:mm:ss |
01:00:00 |
||||||
|
Output frequency |
1 hertz |
||||||
|
eCall location |
Any specified land point between latitude range 80°N and 80°S in coordinate system WGS-84 |
||||||
|
Troposphere: |
Standard predefined model by the GNSS simulator |
||||||
|
Ionosphere: |
Standard predefined model by the GNSS simulator |
||||||
|
PDOP value in the test interval |
2,0 ≤ PDOP ≤ 2,5 |
||||||
|
Simulated signals |
|
||||||
|
Signal strength: |
|
||||||
|
minus 135 dBm; |
||||||
|
minus 138,5 dBm. |
||||||
|
Number of simulated satellites: |
|
2.2.2. Assessment of positioning accuracy in autonomous static mode.
|
(1) |
ΔB(j) = B(j) – Btruej , |
|
(2) |
|
|
(3) |
|
|
(4-1) |
|
|
(4-2) |
|
|
(5-1) |
|
|
(5-2) |
|
|
(6) |
|
2.2.3. Assessment of positioning accuracy in autonomous dynamic mode.
|
Simulated parameter |
Value |
||||||
|
Test duration, hh:mm:ss |
01:00:00 |
||||||
|
Output frequency |
1 hertz |
||||||
|
eCall location |
Any specified land point between latitude range 80°N and 80°S in coordinate system WGS-84 |
||||||
|
Model of movement: |
Manoeuvring movement |
||||||
|
140 |
||||||
|
500 |
||||||
|
0,2 |
||||||
|
Troposphere: |
Standard predefined model by the GNSS simulator |
||||||
|
Ionosphere: |
Standard predefined model by the GNSS simulator |
||||||
|
PDOP value in the test time interval |
2,0 ≤ PDOP ≤ 2,5 |
||||||
|
Simulated signals |
Combined Galileo/GPS/SBAS |
||||||
|
Signal strength: |
|
||||||
|
minus 135 dBm; |
||||||
|
minus 138,5 dBm. |
||||||
|
Number of simulated satellites: |
|
2.2.4. Movement in shadow areas, areas of intermittent reception of navigation signals and urban canyons.
|
Simulated parameter |
Value |
||||||
|
Test duration, hh:mm:ss |
01:00:00 |
||||||
|
Output frequency |
1 hertz |
||||||
|
eCall location |
Any specified land point between latitude range 80°N and 80°S in coordinate system WGS-84 |
||||||
|
Model of movement: |
Manoeuvring movement |
||||||
|
140 |
||||||
|
500 |
||||||
|
0,2 |
||||||
|
Satellite visibility: |
|
||||||
|
300 |
||||||
|
600 |
||||||
|
Troposphere: |
Standard predefined model by the GNSS simulator |
||||||
|
Ionosphere: |
Standard predefined model by the GNSS simulator |
||||||
|
PDOP value in the test time interval |
3,5 ≤ PDOP ≤ 4,0 |
||||||
|
Simulated signals |
Combined Galileo/GPS/SBAS |
||||||
|
Signal strength: |
|
||||||
|
minus 135 dBm; |
||||||
|
minus 138,5 dBm. |
||||||
|
Number of simulated satellites: |
|
Figure 3
Urban canyon definition
|
Zone |
Elevation range (degrees) |
Azimuth range (degrees) |
|
A |
0 – 5 |
0 – 360 |
|
B |
5 – 30 |
210 – 330 |
|
C |
5 – 30 |
30 – 150 |
|
Background |
Area out of Zone A, B, C |
|
|
|
0 dB |
|
B |
– 40 dB |
|
C |
– 40 dB |
|
A |
– 100 dB or signal is switched off |
2.2.5. Cold start time to first fix test.
2.2.6. Test of re-acquisition time of tracking signals after block out of 60 seconds.
2.2.7. Test of GNSS receiver sensitivity in cold start mode, tracking mode, and re-acquisition scenario.
Figure 4
Diagram of path calibration
Figure 5
Arrangement for evaluation of GNSS module sensitivity
ANNEX VII
In-vehicle system self-test
1. Requirements
1.2. Performance requirements
1.3. Documentation requirements
|
Item |
Technical principle applied for monitoring |
|
eCall ECU is in working order (e.g. no internal hardware failure, processor/memory is ready, logic function in expected default state) |
|
|
External mobile network antenna is connected |
|
|
Mobile network communication device is in working order (no internal hardware failure, responsive) |
|
|
External GNSS antenna is connected |
|
|
GNSS receiver is in working order (no internal hardware failure, output within expected range) |
|
|
Crash control unit is connected |
|
|
No communication failures (bus connection failures) of relevant components in this table |
|
|
SIM is present (this item only applies if a removable SIM is used) |
|
|
Power source is connected |
|
|
Power source has sufficient charge (threshold at the discretion of the manufacturer) |
|