Technical Provisions for Mode S Services and Extended Squitter

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DRAFT - Working Paper ASP TSGWP11-01 for review by the TSG during the meeting in June 2011 in Paris C-90 Technical Provisions for Mode S Services and Extended Squitter Version 0 Message TYPE CODE Table C-43. Type Code to NACP Mapping Message Format Position Error (95%) ADS-B Report NACP value 0 No Position Info Unknown 0 5 Surface Position < 3 m 11 6 Surface Position < 10 m 10 7 Surface Position < 0.05 NM 8 8 Surface Position > 0.05 NM 0 9 Airborne Position < 3 m 11 10 Airborne Position < 10 m 10 11 Airborne Position < 0.05 NM 8 12 Airborne Position < 0.1 NM 7 13 Airborne Position < 0.25 NM 6 14 Airborne Position < 0.5 NM 5 15 Airborne Position < 1 NM 4 16 Airborne Position < 5 NM 1 17 Airborne Position < 10 NM 1 18 Airborne Position > 10 NM 0 20 Airborne Position < 4 m 11 21 Airborne Position < 15 m 10 22 Airborne Position > 15 m 0 Note.— The Position Error column of the table indicates the greater of the horizontal or vertical 95% containment radius as listed in Table C-41 for ADS-B Version Zero (0) messages. C.5.2.2.11 Navigation Accuracy Category for Velocity (NACV) The ADS-B Version Zero (0) Airborne Velocity Message (see Table A-2-9a and Table A-2-9b) includes a subfield that conveys the Navigation Uncertainty Category for Velocity (NUCR). The received value of NUCR will shall be mapped directly one-for-one to the Navigation Accuracy Category for Velocity (NACV) field of an ADS-B Report. Draft C.5.2.2.12 Source Integrity Level (SIL) The Source Integrity Level (SIL) defines the probability of the integrity containment region described by the NIC parameter being exceeded for the selected geometric position source, including any external signals used by the source. The value of SIL can only be inferred from the information conveyed in ADS-B Version Zero (0) Messages. Table C-44 shall be used to provides the mapping between the message TYPE Code for a ADS-B Version Zero (0) Transmitting Subsystem and the value of SIL to be reported by a ADS-B Version Two (2) Receiving Subsystem within the ADS-B Report. DRAFT - Working Paper ASP TSGWP11-01 for review by the TSG during the meeting in June 2011 in Paris
DRAFT - Working Paper ASP TSGWP11-01 for review by the TSG during the meeting in June 2011 in Paris Appendix C C-91 Version 0 Message TYPE CODE Message Format Table C-44. SIL Reporting Probability of Exceeding the Horizontal Containment Radius (RC) ADS-B Report SIL value 0 No Position Info No Integrity 0 5 Surface Position 1 X 10 -5 per flight hour or per sample 2 6 Surface Position 1 X 10 -5 per flight hour or per sample 2 7 Surface Position 1 X 10 -5 per flight hour or per sample 2 8 Surface Position 1 X 10 -5 per flight hour or per sample 2 9 Airborne Position 1 X 10 -5 per flight hour or per sample 2 10 Airborne Position 1 X 10 -5 per flight hour or per sample 2 11 Airborne Position 1 X 10 -5 per flight hour or per sample 2 12 Airborne Position 1 X 10 -5 per flight hour or per sample 2 13 Airborne Position 1 X 10 -5 per flight hour or per sample 2 14 Airborne Position 1 X 10 -5 per flight hour or per sample 2 15 Airborne Position 1 X 10 -5 per flight hour or per sample 2 16 Airborne Position 1 X 10 -5 per flight hour or per sample 2 17 Airborne Position 1 X 10 -5 per flight hour or per sample 2 18 Airborne Position No Integrity 0 20 Airborne Position 1 X 10 -5 per flight hour or per sample 2 21 Airborne Position 1 X 10 -5 per flight hour or per sample 2 22 Airborne Position No Integrity 0 C.5.2.2.13 Barometric Altitude Integrity Code (NICBARO) The Barometric Altitude Integrity Code (NICBARO) parameter of the ADS-B Report is a 1-bit flag used to indicate if the barometric altitude being reported in the ADS-B Report has been cross-checked against another source of pressure altitude. The ADS-B Version Zero (0) Messages do not include information related to the cross-checking of barometric altitude. Therefore, ADS-B Reports for target aircraft/vehicles broadcasting ADS-B Version Zero (0) Messages will shall not include the NICBARO field in the report. C.5.2.2.14 Track/Heading and Horizontal Reference Direction (HRD) Draft ADS-B Version Zero (0) Airborne Velocity Messages with Subtype equal to 3 or 4 include a “Magnetic Heading Status Bit” as shown in Table A-2-9b. A Version Two (2) 1090 MHz ADS-B Receiving Subsystem, upon receiving an Airborne Velocity Message with a Subtype of 3 or 4, must decode the Magnetic Heading Status Bit to determine if Magnetic Heading Data is “Available.” The ADS-B Receiving Subsystem will shall set the value of the True/Magnetic Heading subfield, as specified in Table C-45. DRAFT - Working Paper ASP TSGWP11-01 for review by the TSG during the meeting in June 2011 in Paris
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Appendix A A-7 TYPE Code Format Hor
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Appendix A A-13 The supersonic vers
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Appendix A A-97 a) the PI sends a T
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Appendix A A-99 This subfield shall
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Appendix A A-101 These channels hav
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Appendix A A-109 A.4. MODE S BROADC
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Appendix A A-111 Note 1.— This st
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Appendix B B-3 TYPE code Subtype co
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Appendix B B-17 Coding (Binary) (De
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Appendix B B-19 a) ACAS operational
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Appendix B B-21 Subfield Coding: DR
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Appendix B B-41 CF value ICAO/Mode
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Msg Bit # “ME” Bit # Appendix C
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