Technical Provisions for Mode S Services and Extended Squitter

More documents

Recommendations

Info

DRAFT - Working Paper ASP TSGWP11-01 for review by the TSG during the meeting in June 2011 in Paris CD-16 Technical Provisions for Mode S Services and Extended Squitter The A320 (see Table CD-3) has two additional modes compared to the A330/A340: • The Expedite Mode: it climbs or descends at, respectively, “green dot” speed or Vmax speed. • The Immediate Mode: it climbs or descends immediately while respecting the FMS constraints. CD.2.4.4.2.1.3 Synthesis Tables CD-2 and CD-3 show the following: a) Depending on the AP/FD vertical modes and some conditions, the desired “target” altitude might differ. Therefore a logical software combination should be developed in order to load the appropriate parameter in transponder register 4016 with its associated source bit value and status. b) A large number of parameter values are required to implement the logic: the V/S, the FCU ALT, the A/C ALT, the FPA, the FMS ALT and the AP/FD status and vertical modes. The following labels might provide the necessary information to satisfy this requirement: 1. V/S: label 212 (Vertical Rate) from ADC 2. FCU ALT: label 102 from FCC (Selected Altitude) 3. A/C ALT: label 361 from IRS/ADIRS (Inertial Altitude) 4. FPA: label 322 from FMC (Flight Path Angle) 5. FMS ALT: label 102 from FMC (Selected Altitude) 6. AP/FD: labels 272 273 (Arm modes) and 274 (Pitch modes). (Auto-throttle modes), Draft The appropriate “target” altitude should, whatever its nature (A/C, FMS or FCU), be included in a dedicated label (e.g. 271) which would be received by the GFM that will then include it in transponder register 4016. A dedicated label (such as label 271) could then contain the information on the source bits for target altitude. This is demonstrated graphically in Figure C-3. DRAFT - Working Paper ASP TSGWP11-01 for review by the TSG during the meeting in June 2011 in Paris
Appendix CD CD-17 AP/FD mode V/S-FPA value FMS ALT A/C ALT AP/FD status FCU ALT DRAFT - Working Paper ASP TSGWP11-01 for review by the TSG during the meeting in June 2011 in Paris Figure CD-3. Logic to derive the target altitude data information D.2.4.4.2.2 Selected altitude from the altitude control panel When selected altitude from the altitude control panel is provided in bits 1 to 13, the status and mode bits (48 – 51) may be provided from the following sources: Status of altitude control panel mode bits (bit 48) Managed vertical mode (bit 49) Label 274 bit 11 (climb) Label 274 bit 12 (descent) Bus FMGC A Altitude hold mode (bit 50) Label 274 bit 19 (Alt mode) Bus FMGC A Approach mode (bit 51) Label 273 bit 23 Bus AFS FCU A320 A340 SSM labels 273/274 SSM labels 274/275 Label 275 bit 11 (climb) Label 275 bit 15 (descent) Bus FMGEC G GE-1 Label 275 bit 20 (Alt hold) Bus FMGEC G GE-1 Label 273 bit 15 Bus AFS FCU Draft CD.2.4.4.3 TRANSPONDER REGISTER NUMBER 4016 ON BOEING 747-400, 757 AND 767 AIRCRAFT In order to clarify how selected altitude information from the altitude control panel and target altitude is reported in transponder register 4016, a mapping has been prepared to illustrate how the status and mode bits can be derived. Transponder register bit no. Description Label 48 Status of mode bits SSM of 272 and 273 49 Managed vertical mode 272 bit 13 50 Altitude hold mode 272 bit 9 / 273 bit 19 51 Approach mode 272 bit 9 / 273 bit 19 54 Status of target altitude source bits SSM of new label (TBD) 55 56 LOGIC Target altitude (label TBD) Target altitude source bits (label 271) Target altitude source bits New label (TBD) General format manager (GFM) DRAFT - Working Paper ASP TSGWP11-01 for review by the TSG during the meeting in June 2011 in Paris
Page 1 and 2:
DRAFT - Working Paper ASP TSGWP11-0
Page 3 and 4:
Page 5 and 6:
Page 7 and 8:
Page 9 and 10:
Page 11 and 12:
Page 13 and 14:
Page 15 and 16:
Page 17 and 18:
Page 19 and 20:
Page 21 and 22:
Page 23 and 24:
Page 25 and 26:
Page 27 and 28:
Page 29 and 30:
Page 31 and 32:
Appendix A A-7 TYPE Code Format Hor
Page 33 and 34:
Page 35 and 36:
Page 37 and 38:
Appendix A A-13 The supersonic vers
Page 39 and 40:
Appendix A A-15 The transponder sha
Page 41 and 42:
Page 43 and 44:
Page 45 and 46:
Page 47 and 48:
Page 49 and 50:
Page 51 and 52:
Page 53 and 54:
Page 55 and 56:
Page 57 and 58:
Page 59 and 60:
Page 61 and 62:
Page 63 and 64:
Page 65 and 66:
Appendix A A-41 MB FIELD DRAFT - Wo
Page 67 and 68:
Appendix A A-43 MB FIELD 1 MSB TRAN
Page 69 and 70:
Page 71 and 72:
Appendix A A-47 MB FIELD 1 2 3 4 5
Page 73 and 74:
Page 75 and 76:
Page 77 and 78:
Page 79 and 80:
Appendix A A-55 MB FIELD 1 BDS A,8
Page 81 and 82:
Page 83 and 84:
Page 85 and 86:
Page 87 and 88:
Page 89 and 90:
Page 91 and 92:
Page 93 and 94:
Page 95 and 96:
Page 97 and 98:
Page 99 and 100:
Page 101 and 102:
Page 103 and 104:
Page 105 and 106:
Page 107 and 108:
Page 109 and 110:
Page 111 and 112:
Page 113 and 114:
Page 115 and 116:
Page 117 and 118:
Page 119 and 120:
Page 121 and 122:
Appendix A A-97 a) the PI sends a T
Page 123 and 124:
Appendix A A-99 This subfield shall
Page 125 and 126:
Appendix A A-101 These channels hav
Page 127 and 128:
Page 129 and 130:
Page 131 and 132:
Page 133 and 134:
Appendix A A-109 A.4. MODE S BROADC
Page 135 and 136:
Appendix A A-111 Note 1.— This st
Page 137 and 138:
Page 139 and 140:
Appendix B B-3 TYPE code Subtype co
Page 141 and 142:
Page 143 and 144:
Page 145 and 146:
Page 147 and 148:
Page 149 and 150:
Page 151 and 152:
Page 153 and 154:
Appendix B B-17 Coding (Binary) (De
Page 155 and 156:
Appendix B B-19 a) ACAS operational
Page 157 and 158:
Appendix B B-21 Subfield Coding: DR
Page 159 and 160:
Appendix B B-23 Coding (Binary) (De
Page 161 and 162:
Page 163 and 164:
Page 165 and 166:
Page 167 and 168:
Page 169 and 170:
Appendix B B-33 MB FIELD DRAFT - Wo
Page 171 and 172:
Page 173 and 174:
Page 175 and 176:
Page 177 and 178:
Appendix B B-41 CF value ICAO/Mode
Page 179 and 180:
Page 181 and 182:
Page 183 and 184:
Page 185 and 186:
Page 187 and 188:
Page 189 and 190:
Page 191 and 192:
Page 193 and 194:
Appendix C C-5 Table C-2. “TYPE
Page 195 and 196:
Page 197 and 198:
Page 199 and 200:
Appendix C C-11 C.2.3.2.2 Time Sync
Page 201 and 202:
Page 203 and 204:
Page 205 and 206:
Page 207 and 208:
Page 209 and 210:
Page 211 and 212:
Page 213 and 214:
Appendix C C-25 Notes.— DRAFT - W
Page 215 and 216:
Page 217 and 218:
Page 219 and 220:
Msg Bit # “ME” Bit # Appendix C
Page 221 and 222:
Appendix C C-33 Msg Bit # "ME” Bi
Page 223 and 224:
Page 225 and 226:
Page 227 and 228:
Page 229 and 230:
Page 231 and 232:
Appendix C C-43 Notes. — DRAFT -
Page 233 and 234:
Page 235 and 236:
Page 237 and 238:
Page 239 and 240:
Appendix C C-51 3. The decoded posi
Page 241 and 242:
Page 243 and 244:
Page 245 and 246:
Appendix C C-57 B Reports to have k
Page 247 and 248:
Appendix C C-59 Register 0516 DRAFT
Page 249 and 250: Appendix C C-61 Register 0716 DRAFT
Page 253 and 254: Appendix C C-65 Register 0A16 Figur
Page 255 and 256: DRAFT - Working Paper ASP TSGWP11-0
Page 259 and 260: Appendix C C-71 Table C-37. CF Fiel
Page 287 and 288: Appendix CD CD-3 ACTIONS EVENTS DRA
Page 291 and 292: Appendix CD CD-7 too many broadcast
Page 297 and 298: Appendix CD CD-13 CD.2.4.4.1.2 Poss
Page 299: Appendix CD CD-15 D.2.4.4.2.1.2 A32
Page 307 and 308: Appendix CD CD-23 CD.2.4.7.5 BINARY
Page 311 and 312: Appendix CD CD-27 Zone no. DRAFT -
Page 315 and 316: Appendix CD CD-31 CD.4 IMPLEMENTATI
Page 325 and 326: Appendix DE DE-7 c. for GNSS, the p
Page 327 and 328: Appendix DE DE-9 MB FIELD DRAFT - W
Page 329 and 330: Appendix DE DE-11 MB FIELD DRAFT -
show all

Technical Provisions for Mode S Services and Extended Squitter

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

Delete template?

Save as template?