Minimum Aviation System Performance Standards for Aircraft ...

More documents

Recommendations

Info

86 © 20xx, RTCA, Inc. a. The ADS-B Transmitting Subsystem shall (242AR3.147-B) accept information from an appropriate interface that indicates whether or not the Altitude Hold Mode is active. b. The ADS-B Transmitting Subsystem shall (242AR3.147-C) set the Mode Indicator: Altitude Hold Mode field in accordance with Table 3.2.28. Table 3.2.28: “Mode Indicator: Altitude Hold Mode” Field Values Values Meaning 0 Altitude Hold Mode is NOT Active or Unknown 1 Altitude Hold Mode is Active 3.2.29 Mode Indicator: Approach Mode Field The “Mode Indicator: Approach Mode” is a 1-bit field that shall (242AR3.148-A) be used to indicate whether the Approach Mode is active or not. a. The ADS-B Transmitting Subsystem shall (242AR3.148-B) accept information from an appropriate interface that indicates whether or not the Approach Mode is active. b. The ADS-B Transmitting Subsystem shall (242AR3.148-C) set the Mode Indicator: Approach Mode field in accordance with Table 3.2.29. Table 3.2.29: “Mode Indicator: Approach Mode” Field Values Values Meaning 0 Approach Mode is NOT Active or Unknown 1 Approach Mode is Active 3.2.30 Mode Indicator: LNAV Mode Engaged Field The “Mode Indicator: LNAV Mode Engaged” is a 1-bit field that shall (242AR3.149-A) be used to indicate whether the Lateral Navigation Mode is active or not. a. The ADS-B Transmitting Subsystem shall (242AR3.149-B) accept information from an appropriate interface that indicates whether or not the Lateral Navigation Mode is active. b. The ADS-B Transmitting Subsystem shall (242AR3.149-C) set the Mode Indicator: LNAV Mode Engaged field in accordance with Table 3.2.30. Table 3.2.30: “Mode Indicator: LNAV Mode Engaged” Field Values Values Meaning 0 LNAV Mode is NOT Active 1 LNAV Mode is Active
3.3 System Application Requirements 3.4 Subsystem Requirements 3.4.1 Subsystem Requirements for ASSAP (Dave Elliott) ASSAP is the surveillance and separation assurance processing component of ASA. ASSAP processes incoming data from own-ship, and other aircraft/vehicles (A/V), and derives information for display on the CDTI. Flight crew command and control inputs that affect application functions are also processed by ASSAP. In the future, ASSAP is expected to provide alerting and guidance information to the flight crew via the CDTI. The two major functions of ASSAP are surveillance processing and applications processing. Functional requirements for ASSAP are described in §3.4.1.4. Surveillance processing: • Establishes tracks from ADS-B, ADS-R, and TIS-B traffic reports • Cross-references traffic from different surveillance sources (ADS-B, ADS-R, TIS-B, and TCAS) • Estimates track state (e.g., position, velocity), and track quality • Deletes tracks that are beyond the maximum allowable coast time for any ASA applications Applications processing: • Determines the appropriateness of track information for various applications, and forwards the track data to the CDTI • May performs alerting functions in future applications • May derive guidance information in future applications Each ASA transmit participant should input to ASSAP the highest quality state data that is available on-board; this information should be the same as that used for ADS-B transmission. ASSAP assesses own-ship performance and transmitted data quality as specified in Table x.y and assesses received traffic data quality as specified in Table x.y to determine if an active application can be supported. Figure 3.4.1 summarizes ASSAP input / output interfaces to other subsystems and indicates the sections where the interface, functional, and performance requirements can be found in this document. © 20xx, RTCA, Inc. 87
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:
3.3.23 Selected Heading Sign Field.
Page 9 and 10:
LIST OF TABLES Table 2-5: High Leve
Page 11:
This Page Intentionally Left Blank.
Page 14 and 15:
2 © 20xx, RTCA, Inc. C: Derivation
Page 16 and 17:
4 1.2.3 ASA Architecture © 20xx, R
Page 18 and 19:
6 © 20xx, RTCA, Inc. The TCAS traf
Page 20 and 21:
8 © 20xx, RTCA, Inc. DO-3xx ADS-B
Page 22 and 23:
10 1.3.1.4 Basic Surface Situationa
Page 24 and 25:
12 2 Operational Requirements 2.1 G
Page 26 and 27:
14 © 20xx, RTCA, Inc. timeliness,
Page 28 and 29:
16 © 20xx, RTCA, Inc. Table 2-6: R
Page 30 and 31:
18 2. FAA TSO-C195 states applicati
Page 32 and 33:
20 © 20xx, RTCA, Inc. Notes for Ta
Page 34 and 35:
22 © 20xx, RTCA, Inc. • Optimiza
Page 36 and 37:
24 © 20xx, RTCA, Inc. same approac
Page 38 and 39:
26 © 20xx, RTCA, Inc. may allow de
Page 40 and 41:
28 © 20xx, RTCA, Inc. An aircraft
Page 42 and 43:
30 Information ↓ Initial Acquisit
Page 44 and 45:
32 © 20xx, RTCA, Inc. NRA - 3 NM E
Page 46 and 47:
34 © 20xx, RTCA, Inc. Aircraft typ
Page 48 and 49: 36 © 20xx, RTCA, Inc. This Page In
Page 50 and 51: 38 © 20xx, RTCA, Inc. In Figure 3.
Page 52 and 53: 40 © 20xx, RTCA, Inc. Figure 3.1.1
Page 54 and 55: 42 3.1.1.1.3 Functional Level © 20
Page 58 and 59: 46 © 20xx, RTCA, Inc. Table 3.1.1.
Page 62 and 63: 50 © 20xx, RTCA, Inc. Figure 3-8 i
Page 64 and 65: 52 USER AIR INTERFACE © 20xx, RTCA
Page 66 and 67: 54 3.1.4.2.1.4 ADS-R in Enroute and
Page 68 and 69: 56 TIS‐B Non‐Equipped © 20xx,
Page 70 and 71: 58 © 20xx, RTCA, Inc. available fo
Page 72 and 73: 60 3.2.2 Identification 3.2.2.1 Cal
Page 74 and 75: 62 © 20xx, RTCA, Inc. i. Lighter-t
Page 76 and 77: 64 © 20xx, RTCA, Inc. The ADS-B po
Page 78 and 79: 66 3.2.4.2 Altitude © 20xx, RTCA,
Page 80 and 81: 68 3.2.7 Heading © 20xx, RTCA, Inc
Page 82 and 83: 70 3.2.8.7 Other Capability Codes
Page 84 and 85: 72 SDA Value (decimal) (binary) 0 0
Page 86 and 87: 74 © 20xx, RTCA, Inc. Table 3.2.9.
Page 88 and 89: 76 © 20xx, RTCA, Inc. 5. RC < 0.3
Page 90 and 91: 78 © 20xx, RTCA, Inc. Table 3.2.12
Page 92 and 93: 80 3.2.16 Geometric Vertical Accura
Page 94 and 95: 82 © 20xx, RTCA, Inc. Note: Users
Page 96 and 97: 84 3.2.24 Selected Heading Field ©
Page 100 and 101: 88 3.4.1.1 Definitions © 20xx, RTC
Page 102 and 103: 90 Source Info Category Information
Page 104 and 105: 92 © 20xx, RTCA, Inc. 5. Required
Page 106 and 107: 94 © 20xx, RTCA, Inc. ASSAP shall
Page 108 and 109: 96 3.4.2.2 Latency 3.4.2.3 Integrit
Page 110 and 111: 98 3.4.2.11 Suitability of Traffic
Page 112 and 113: 100 3.4.3.1 ADS-B Surveillance Cove
Page 114 and 115: 102 © 20xx, RTCA, Inc. required to
Page 116 and 117: 104 Equipage Class ↓ B0 Aircraft
Page 118 and 119: © 20xx, RTCA, Inc. Table 3.4.3.3.1
Page 120 and 121: © 20xx, RTCA, Inc. Notes for Table
Page 122 and 123: Operational Domain → © 20xx, RTC
Page 124 and 125: © 20xx, RTCA, Inc. 2. Future versi
Page 126 and 127: © 20xx, RTCA, Inc. • Report time
Page 128 and 129: 3.5.1.2 ADS-B Message Exchange Tech
Page 130 and 131: Notes: © 20xx, RTCA, Inc. 1. It is
Page 132 and 133: © 20xx, RTCA, Inc. • Ground Spee
Page 134 and 135: © 20xx, RTCA, Inc. Note: The recom
Page 136 and 137: 3.5.1.3.12 Heading While on the Sur
Page 138 and 139: 3.5.1.4 Mode Status Report © 20xx,
Page 140 and 141: © 20xx, RTCA, Inc. 3. These elemen
Page 142 and 143: 3.5.1.4.9 Capability Class (CC) Cod
Page 144 and 145: 3.5.1.4.15 Geometric Vertical Accur
Page 146 and 147: 3.5.1.6.2 ARV Report Update Require
Page 148 and 149:
© 20xx, RTCA, Inc. The higher “s
Page 150 and 151:
© 20xx, RTCA, Inc. Whereas ADS-B r
Page 152 and 153:
4 ADS-B IN System Applications Requ
Page 154 and 155:
© 20xx, RTCA, Inc. Broadcast (ADS-
Page 156 and 157:
© 20xx, RTCA, Inc. This Page Inten
Page 158 and 159:
This page intentionally left blank.
Page 160 and 161:
Appendix A Page A-2 ©20xx, RTCA, I
Page 162 and 163:
Page 164 and 165:
Page 166 and 167:
Appendix A Page A-8 A.2 Definitions
Page 168 and 169:
Appendix A Page A-10 Air/Ground Sta
Page 170 and 171:
Appendix A Page A-12 Collision Avoi
Page 172 and 173:
Appendix A Page A-14 Extended Displ
Page 174 and 175:
Appendix A Page A-16 Latency Compen
Page 176 and 177:
Appendix A Page A-18 Regime - Divis
Page 178 and 179:
Appendix A Page A-20 TCAS Potential
Page 180 and 181:
Appendix B Bibliography
Page 182 and 183:
B Bibliography Appendix B Page B-1
Page 184 and 185:
Appendix B Page B-3 Name Reference
Page 186 and 187:
Page 188 and 189:
Page 190 and 191:
Page 192 and 193:
show all

Minimum Aviation System Performance Standards for Aircraft ...

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?