Minimum Aviation System Performance Standards for Aircraft ...

More documents

Recommendations

Info

64 © 20xx, RTCA, Inc. The ADS-B position reference point of an A/V shall (242AR2.18) be defined as the center of a rectangle (the “defining rectangle for position reference point”) that has the following properties: a. The defining rectangle for position reference point shall (242AR2.18-A) have length and width as defined in Table 3.2.4.1a below for the length and width codes that the participant is transmitting in messages to support the MS report. b. The defining rectangle for position reference point shall (242AR2.18-B) be aligned parallel to the A/V’s heading. c. The ADS-B position reference point (the center of the defining rectangle for position reference point) shall (242AR2.18-C) lie along the axis of symmetry of the A/V. (For an asymmetrical A/V, the center of the rectangle should lie midway between the maximum port and starboard extremities of the A/V.) d. The forward extremity of the A/V shall (242AR2.18-D) just touch the forward end of the defining rectangle for position reference point. Table 3.2.4.1a: Dimensions of Defining Rectangle for Position Reference Point. A/V – L/W Code (Decimal) Length Code (binary) Width Code (binary) Upper-Bound Length and Width for Each Length/Width Code Length Width (meters) (meters) 0 0 0 0 0 No Data or Unknown 1 0 0 0 1 15 23 2 3 0 0 1 0 1 25 28.5 34 4 5 0 1 0 0 1 35 33 38 6 7 0 1 1 0 1 45 39.5 45 8 9 1 0 0 0 1 55 45 52 10 11 1 0 1 0 1 65 59.5 67 12 13 1 1 0 0 1 75 72.5 80 14 15 1 1 1 0 1 85 80 90 Note 2: The lengths and widths given in Table 3.2.4.1a are least upper bounds for the possible lengths and widths of an aircraft that reports the given length and width code as specified in Table TBD (§3.5.4.6). An exception, however, is made for the largest length and width codes, since there is no upper bound for the size of an aircraft that broadcasts those largest length and width codes. Figure 3.2.4.1a illustrates the location of the ADS-B reference point, for an example aircraft of length 31 m and width 29 m. Such an aircraft will have length code 2 (L < 35 m) and width code 0 (W < 33m). The ADS-B position reference point is then the center
of a rectangle that is 35 m long and 33 m wide and positioned as given in the requirements just stated. As required in §2.1.2.3, this is the position that a transmitting ADS-B participant broadcasts when its “reporting reference point position” CC code is ONE. Actual aircraft length is 31 m Reported Width = 33 m Actual Aircraft width is 29 m The defining rectangle for the position reference point has the least-upper bound length and width (35 m and 33 m respectively) for the aircraft's length and width codes. This defining rectangle should touch the aircraft's forward end. The ADS-B position reference point is at the center of its defining rectangle. Center of larger rectangle (that is, ADS-B position reference point) lies on the centerline of the smaller, circumscribing rectangle (which is almost always the axis of symmetry of the aircraft). Figure 3.2.4.1a: Position Reference Point Definition. Note 3: When on the surface, the ability to correct for inaccuracies due to offsets in position between the navigation sensor and the ADS-B position reference point must be provided. If the navigation sensor or the transmitting ADS-B participant does not correct for this offset, the lateral distance from the lateral axis of the aircraft and the longitudinal distance from the nose of the aircraft must be conveyed so that the ADS-B application can account for this offset. A means to indicate that the position is corrected to the ADS-B reference point must be provided. � Editor’s Note: Add reference to the GPS Antenna Offset section below. � © 20xx, RTCA, Inc. 65 Reported Length = 35 m
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 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 98 and 99: 86 © 20xx, RTCA, Inc. a. The ADS-B
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 ...

Create successful ePaper yourself

Delete template?

Save as template?