Minimum Aviation System Performance Standards for Aircraft ...

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16 © 20xx, RTCA, Inc. Table 2-5: High Level Considerations for ADS-B In Applications by Category 1 SA Applications 2 "Enhanced SA" Applications 3 Spacing Apps 4 Delegated Separation Applications 5 Self Separation Airborne Approach Surface Oceanic Approach Surface EnRoute / Terminal EnRoute / Terminal EnRoute / Terminal Requirement AIRB VSA SURF ITP CAVS/ CEDS SURF IA FIM-S Advanced FIM-DS DS-C/P ICSPA DSWRM FC Self Sep Separation Responsibility ATC (1) ATC (1, 2) ATC (1) ATC ATC ATC ATC ATC Shared Shared Shared Shared Aircraft Aircraft 100% OUT Equipage? (Direct, ADS-R or TIS-B) No No No No No No No No TBD TBD TBD TBD TBD TBD 100% IN / CDTI Equipage? No No No No No No No No TBD TBD TBD TBD TBD TBD Operational Conditions TBD VMC Only No Reqmt VMC / IMC VMC / IMC No Reqmt VMC / IMC VMC / IMC VMC / IMC VMC / IMC VMC / IMC VMC / IMC VMC / IMC VMC / IMC 3D / 4D Intent Data? No No No No No No TBD TBD TBD TBD TBD TBD Yes Yes Wake Vortex Data? No No No No No No No No No TBD TBD Yes TBD TBD Increased Perf Levels? (3) (> FAA 2020 Mandate) No No Yes No TBD Yes TBD TBD TBD TBD TBD TBD TBD TBD Notes: 1. Only when aircraft is on IFR Flight Plan. 2. ATC for all aircraft except ATC designated traffic to follow. 3. Performance level used for comparison is that of FAA Final ADS-B OUT Rule and AC 20-165 (Ref TBD). 4. Red highlighting means that there may be a problem meeting the minimum performance requirements of the application. 5. Yellow highlighting means that the requirements are not defined.
Airborne Situational Awareness (AIRB) Table 2-6: Required Information Elements to Support Selected ADS-B Applications Enhanced Situational Awareness (ITP) Spacing (FIM-S) Delegated Separation Assurance & Sequencing (FIM-DS) Simultaneous Approaches (DS) Airport Surface (A/V to A/V & A/V to ATS) Self Separation ATS Surveillance ADS-B OUT Traffic Situation Awareness W/Alerts (TSAA) Notes Information Element � Identification Flight ID (Call Sign) � � � � � � � 1 Address � � � � � � � � � Category � � � � � Mode A Code State Vector � Horizontal Position � � � � � � � � � Vertical Position � � � � � � � � Horizontal Velocity � � � � � � � � Vertical Velocity � � � � � � � � Surface Heading � Ground Speed � NIC Mode Status � � � � � � � � Emergency/ Priority Status � � � � Capability Codes � � � � � � � � Operational Modes � � � � � � � � NACP � � � � � � � � � NACV � � � � � � � � SIL � � � � � � � � SDA � � � � � � � � � ARV TBD Intent Data (Note 1) TBD TBD TBD Notes for Table 2-6: • = Expected Application Requirement 1. ADS-B is one potential means to provide intent information to support ATS. Other alternatives, not involving ADS-B, may become available. © 20xx, RTCA, Inc. 17
Page 1 and 2: 1150 18 th Street, NW, Suite 910 Wa
Page 3 and 4: FOREWORD This document was prepared
Page 5 and 6: TABLE OF CONTENTS 1 PURPOSE AND SCO
Page 7 and 8: 3.2.25 Status of MCP/FCU Mode Bits
Page 9 and 10: APPENDICES Appendix A Acronyms and
Page 11 and 12: Table 3.4.3.1b: Interoperability Ra
Page 13 and 14: 1 PURPOSE AND SCOPE 1.1 Introductio
Page 15 and 16: � Enabling aircraft in oceanic ai
Page 17 and 18: is minimizing the latency between t
Page 19 and 20: uses of TCAS and ASA, and in partic
Page 21 and 22: provision is still the controller's
Page 23 and 24: The ADS-B system scope is the middl
Page 25 and 26: 2 Operational Requirements 2.1 Gene
Page 27: The following subsections describe
Page 31 and 32: Notes for Table 2-7: 1. The airborn
Page 33 and 34: Notes for Table 2-8: 1. System must
Page 35 and 36: this new distance-based longitudina
Page 37 and 38: � Mechanisms for aircraft-aircraf
Page 39 and 40: the lead and other proximate aircra
Page 41 and 42: environment there is a need to supp
Page 43 and 44: Operational Scenarios Blind Taxi: T
Page 45 and 46: Table 2-9(b): Additional Expected C
Page 47 and 48: Scenario � NRA - 5 NM EnRoute Tab
Page 49 and 50: Aircraft type classification, statu
Page 51 and 52: 3 ADS-B and Airborne Systems Defini
Page 53 and 54: Participant - N Participant - 2 Par
Page 55 and 56: ADS-B Message Generation Function A
Page 57 and 58: certification process. The distribu
Page 59 and 60: own-aircraft’s air crew). This eq
Page 61 and 62: Class C2: Ground ATS Receive-Only A
Page 63 and 64: 3.1.3 CDTI Subsystem Description Th
Page 65 and 66: . Approach Control Service 2. Fligh
Page 67 and 68: 3.1.4.2.1 ADS-R Service Figure 3-8:
Page 69 and 70: USER AIR INTERFACE ADS-B MESSAGES R
Page 71 and 72: 3.1.4.2.1.4 ADS-R in Enroute and Te
Page 73 and 74: TIS‐B Non‐Equipped UAT FIS‐B
Page 75 and 76: available for a Mode S track (typic
Page 77 and 78: Three squitters (even position, odd
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TIS-B Message Encoding Used Based o
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The TIS-B/ADS-R Service Status mess
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3.1.4.3.1.2.2 TIS-B Position Update
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UAT transmissions shall be randomiz
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The nominal message transmission ra
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UAT transmissions shall be randomiz
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aircraft/vehicle addresses shall {2
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3.2.2.4 Mode 3/A Code Since the Mod
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Table 3.2.4.1a: Dimensions of Defin
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3.2.4.2 Altitude means to indicate
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3.2.7 Heading 4. Pure barometric ra
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3.2.8.6 UAT Receive Capability The
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SDA Value (decimal) (binary) 0 00 T
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Table 3.2.9.6B: Longitudinal Axis G
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It is recommended that the coded re
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Table 3.2.12a: Navigation Accuracy
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3.2.16 Geometric Vertical Accuracy
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101 of the airplane during certain
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3.2.24 Selected Heading Field a. Th
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105 a. The ADS-B Transmitting Subsy
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Figure 3-15: End to End ASA System
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3.3.1.2.2 Interface A2 3.3.1.2.3 In
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111 The CDTI function may translate
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113 The update interval of ADS-R or
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data extrapolated to a common time
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Source Info Category Information El
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If the ASSAP determines that multip
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121 The operating range of display
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3.4.2.9 Multi-Function Display (MFD
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3.4.3 Subsystem Requirements for AD
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Table 3.4.3.1b: Interoperability Ra
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Equipage Class � B0 Aircraft R�
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Table 3.4.3.3.1.1a shows accuracy v
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2. The analysis in RTCA DO-242A, Ap
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2. The 90 NM range requirement appl
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Table 3.4.3.3.1.3a: Summary of TS R
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Instaneous air count 800 700 600 50
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Growth Factor GNY( ma �� ) ( 1
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Where the ADS-B System is used as a
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eliability required for the intende
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its component information is receiv
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c. Lighter Than Air d. Unmanned Aer
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. ADS-B participants that are known
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3.5.1.3.6 Geometric Altitude Field
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3. For operations at some airports,
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MS Elem. # Table 3.5.1.4: Mode Stat
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3.5.1.4.5 Emitter Category Field An
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3.5.1.4.11 Navigation Accuracy Cate
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3.5.1.6 Air Referenced Velocity (AR
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3.5.1.6.7 Heading Valid Field The
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3.5.1.7.9 MCP/FCU Mode Indicator: V
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alternate position sources may not
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3.6.4 TCAS The heading data will in
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3.6.5.3 Reference Datum The airport
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application-unique processing and d
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Figure 4-2: Example for SURF IA Ind
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This Page Intentionally Left Blank.
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This page intentionally left blank.
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Appendix A Page A-2 ©20xx, RTCA, I
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Page 201 and 202:
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Appendix A Page A-8 A.2 Definitions
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Appendix A Page A-10 Air/Ground Sta
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Appendix A Page A-12 Collision Avoi
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Appendix A Page A-14 Extended Displ
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Appendix A Page A-16 Latency Compen
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Appendix A Page A-18 Regime - Divis
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Appendix A Page A-20 Target State R
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Appendix A Page A-22 DO-3xx Reqmts
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Appendix A Page A-24 DO-3xx Reqmts
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Appendix B Page B-2 [15] RTCA, Traf
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Appendix B Page B-4 [44] RTCA, Safe
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C Derivation of Link Quality Requir
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C.3.4 Altitude Accuracy The fundame
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The Page Intentionally Left Blank.
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Appendix F Page F-2 F.1.2 ADS-B Tra
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Appendix F Page F-4 F.2.2 Design Al
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Appendix F Page F-6 F.3.2 Performan
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Appendix F Page F-8 © 20xx RTCA, I
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Appendix F Page F-10 © 20xx RTCA,
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Appendix F Page F-12 1 0.9 0.8 0.7
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Appendix F Page F-14 © 20xx RTCA,
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Appendix G Page G-2 North Position
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Appendix G Page G-4 ARV information
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Appendix G Page G-6 � 20xx, RTCA,
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