Common use of Position determination Clause in Contracts

Position determination. If the applicant for approval so requests, the position determination can be part of the approval of a type of AECC. In this case, the following provisions shall apply. If the AECC is fitted, in accordance with paragraph 1.4., with GNSS receiver supporting at least three GNSS including GLONASS, Galileo and GPS, and is capable of reception and processing of SBAS signals, then the AECC shall comply with the requirements of paragraphs 7.3.1. to 7.3.11. AECC compliance with respect to positioning capabilities shall be demonstrated by performing test methods described in Annex 10: Test methods for the navigation solutions. 7.3.1. The GNSS receiver shall be able to output the navigation solution in a NMEA-0183 protocol format (RMC, GGA, VTG, GSA and GSV message). The AECC set-up for NMEA-0183 messages output shall be described in the operation manual. 7.3.2. The GNSS receiver being a part of the AECC shall be capable of receiving and processing individual GNSS signals in L1/E1 band from at least three global navigation satellite systems, including GLONASS, GALILEO and GPS. 7.3.3. The GNSS receiver being a part of the AECC shall be capable of receiving and processing combined GNSS signals in L1/E1 band from at least three global navigation satellite systems, including GLONASS, GALILEO, GPS and SBAS. 7.3.4. The GNSS receiver being a part of the AECC shall be able to provide positioning information in WGS-84 coordinate systems. 7.3.5. Horizontal position error shall not exceed: (a) Under open sky conditions: 15 m at a confidence level of 0.95 probability with Position Dilution of Precision (PDOP) in the range from 2.0 to 2.5; (b) In urban canyon conditions: 40 m at a confidence level of 0.95 probability with PDOP in the range from 3.5 to 4. 7.3.6. The specified requirements for accuracy shall be provided at the: (a) Speed range of 0 to 140 km/h; (b) Linear acceleration range of 0 to 2g. 7.3.7. Sensitivity at receiver input shall be: (a) GNSS signals detection (cold start) do not exceed 3,600 s at the signal level on the antenna input of the AECC of minus 144 dBm; (b) GNSS signals tracking and navigation solution calculation is available for at least 600 s at the signal level on the antenna input of the AECC of minus 155 dBm; (c) Re-acquisition of GNSS signals and calculation of the navigation solution is possible and does not exceed 60 s at the signal level on the antenna input of the AECC of minus 150 dBm. 7.3.8. Cold start time to first fix shall not exceed (a) 60 s for a signal level down to minus 130 dBm; (b) 300 s for a signal level down to minus 140 dBm. 7.3.9. GNSS signal re-acquisition time after a block out of 60 s at a signal level down to minus 130 dBm shall not exceed 20 s at the recovery time of the navigation satellite visibility. 7.3.10. The GNSS receiver shall be able to obtain a position fix at least for every second. 7.3.11. The testing procedures in Annex 8 can be performed either on the AECC unit including post-processing ability or directly on the GNSS receiver as a part of the AECC.

Position determination. If the applicant for approval so requests, the position determination can be part of the approval of a type of AECC. In this case, the following provisions shall apply. If the AECC is fitted, in accordance with paragraph 1.4., with GNSS receiver supporting at least three GNSS including GLONASS, Galileo and GPS, and is capable of reception and processing of SBAS signals, then the AECC shall comply with the requirements of paragraphs 7.3.1. to 7.3.11. AECC compliance with respect to positioning capabilities shall be demonstrated by performing test methods described in Annex 10: Test methods for the navigation solutions. 7.3.1. The GNSS receiver shall be able to output the navigation solution in a NMEA-0183 protocol format (RMC, GGA, VTG, GSA and GSV message). The AECC set-up for NMEA-0183 messages output shall be described in the operation manual. 7.3.2. The GNSS receiver being a part of the AECC shall be capable of receiving and processing individual GNSS signals in L1/E1 band from at least three global navigation satellite systems, including GLONASS, GALILEO and GPS. 7.3.3. The GNSS receiver being a part of the AECC shall be capable of receiving and processing combined GNSS signals in L1/E1 band from at least three global navigation satellite systems, including GLONASS, GALILEO, GPS and SBAS. 7.3.4. The GNSS receiver being a part of the AECC shall be able to provide positioning information in WGS-84 coordinate systems. 7.3.5. Horizontal position error shall not exceed: (a) Under open sky conditions: 15 m at a confidence level of 0.95 probability with Position Dilution of Precision (PDOP) in the range from 2.0 to 2.5; (b) In urban canyon conditions: 40 m at a confidence level of 0.95 probability with PDOP in the range from 3.5 to 4. 7.3.6. The specified requirements for accuracy shall be provided at the: (a) Speed range of 0 to 140 km/h; (b) Linear acceleration range of 0 to 2g. 7.3.7. Sensitivity at receiver input shall be: (a) GNSS signals detection (cold start) do not exceed 3,600 s at the signal level on the antenna input of the AECC of minus 144 dBm; (b) GNSS signals tracking and navigation solution calculation is available for at least 600 s at the signal level on the antenna input of the AECC of minus 155 dBm; (c) Re-acquisition of GNSS signals and calculation of the navigation solution is possible and does not exceed 60 s at the signal level on the antenna input of the AECC of minus 150 dBm. 7.3.8. Cold start time to first fix shall not exceed (a) 60 s for a signal level down to minus 130 dBm; (b) 300 s for a signal level down to minus 140 dBm. 7.3.9. GNSS signal re-acquisition time after a block out of 60 s at a signal level down to minus 130 dBm shall not exceed 20 s at the recovery time of the navigation satellite visibility. 7.3.10. The GNSS receiver shall be able to obtain a position fix at least for every second. 7.3.11. The testing procedures in Annex 8 10 can be performed either on the AECC unit including post-processing ability or directly on the GNSS receiver as a part of the AECC.

Position determination. If the applicant for approval so requests, the position determination can be part of the approval of a type of AECC. In this case, the following provisions shall apply. If the AECC is fitted, in accordance with paragraph 1.4., with GNSS receiver supporting at least three GNSS including GLONASS, Galileo and GPS, and is capable of reception and processing of SBAS signals, then the AECC shall comply with the requirements of paragraphs 7.3.1. to 7.3.11. AECC compliance with respect to positioning capabilities shall be demonstrated by performing test methods described in Annex 10: Test methods for the navigation solutions. 7.3.1. The GNSS receiver shall be able to output the navigation solution in a NMEA-0183 NMEA- 0183 protocol format (RMC, GGA, VTG, GSA and GSV message). The AECC set-up for NMEA-0183 messages output shall be described in the operation manual. 7.3.2. The GNSS receiver being a part of the AECC shall be capable of receiving and processing individual GNSS signals in L1/E1 band from at least three global navigation satellite systems, including GLONASS, GALILEO and GPS. 7.3.3. The GNSS receiver being a part of the AECC shall be capable of receiving and processing combined GNSS signals in L1/E1 band from at least three global navigation satellite systems, including GLONASS, GALILEO, GPS and SBAS. 7.3.4. The GNSS receiver being a part of the AECC shall be able to provide positioning information in WGS-84 coordinate systems. 7.3.5. Horizontal position error shall not exceed: (a) Under open sky conditions: 15 m at a confidence level of 0.95 probability with Position Dilution of Precision (PDOP) in the range from 2.0 to 2.5; (b) In urban canyon conditions: 40 m at a confidence level of 0.95 probability with PDOP in the range from 3.5 to 4. 7.3.6. The specified requirements for accuracy shall be provided at the: (a) Speed range of 0 to 140 km/h; (b) Linear acceleration range of 0 to 2g. 7.3.7. Sensitivity at receiver input shall be: (a) GNSS signals detection (cold start) do not exceed 3,600 s at the signal level on the antenna input of the AECC of minus 144 dBm; (b) GNSS signals tracking and navigation solution calculation is available for at least 600 s at the signal level on the antenna input of the AECC of minus 155 dBm; (c) Re-acquisition of GNSS signals and calculation of the navigation solution is possible and does not exceed 60 s at the signal level on the antenna input of the AECC of minus 150 dBm. 7.3.8. Cold start time to first fix shall not exceed (a) 60 s for a signal level down to minus 130 dBm; (b) 300 s for a signal level down to minus 140 dBm. 7.3.9. GNSS signal re-acquisition time after a block out of 60 s at a signal level down to minus 130 dBm shall not exceed 20 s at the recovery time of the navigation satellite visibility. 7.3.10. The GNSS receiver shall be able to obtain a position fix at least for every second. 7.3.11. The testing procedures in Annex 8 10 can be performed either on the AECC unit including post-processing ability or directly on the GNSS receiver as a part of the AECC.