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Table A7-6, Line codes for partial correlation coefficient No. 5
QUANTIZER LINE
LEVEL CODE
-0.538661 0 0000
-0.4685838 0001
-0.3954149 0010
-0.3 196371 001 1
-0.241 7503 0100
-0.1622685 0101
-0.0817161 01 10
-0.0006245 0111
QUANTIZER LINE
LEVEL CODE
0.08047 12 1000
0.1610360 1001
0.2405382 1010
0.3 184534 1011
0.3942675 1100
0.4674802 1101
0.5376085 1110
0.6041 898 1111
Table A7-7. Line codes for partial correlation coefficient No. 6
QUANTIZER
LEVEL
LINE
CODE CODE
Table A7-8. Line codes for partial correlation coefficient No. 7
QUANTIZER LINE
LEVEL CODE
-0.3958643 000
6.26063 14 00 1
-0.1200220 010
0.0230632 011
CODE
Annex 10 - Aeronautical Telecommunications Volume I11
Table A7-9. Line codes for partial correlation coeficient No. 8
Table A7-10. Line codes for partial correlation coefncient No. 9
QUANTIZER QUANTIZER
LEVEL CODE LEVEL
Table A7-11. Line codes for partial correlation coefficient No. 10
QUANTlZER
LEVEL CODE LEVEL
Table A7-12. Line encoding for quantized
long-term predictor qgain
LINE
qgain CODE
Annex 10 - Aeronauticnl Telecommunications
Table A7-13. Line encoding for the
long term predictor delay
delay a
Table A7-14. Line codes for the first and second pulse
amplitudes of each excitation frame
DECISION CONTENTS OF QAMPll J LINE
THRESHOLD AND [2] CODE
Annex 10 - Aeronautical Telecommunications
Table A7-15. Line codes for the third pulse amplitude of
each excitation frame
DECISION CONTENTS OF LINE
THRESHOLD QAMPf3J CODE
Table A7-16. Line codes for the three pulse positions
within each excitation frame
PULSE
POSITION
LINE
CODE
Volume 666
Annex 10 - Aeronautical Tekcommunications
Table A7-17. Transmission frame structure
I FRAME COMPONENT (line code) REFERENCE LENGTH (bits) I
Partial correlation coefficient No. 1
Partial correlation coefficient No. 2
Partial correlation coefficient No. 3
Partial correlation coefficient No. 4
Partial correlation coefficient No. 5
Partial correlation coefficient No. 6
Partial correlation coefficient No. 7
Partial correlation coefficient No. 8
Partial correlation coefficient No. 9
Partial correlation coefficient No. 10
Hamming code word (5 bits plus odd parity)
Burst error detection
Long term correlation gain
Long term correlation delay
Excitation frame No. 1 (pulse no. 1 position)
Excitation framc No. 1 (pulse no. I ampli~ude)
Excitation framc No. 1 (pulse no. 2 position)
Excitation frame No. 1 (pulse no. 2 amplitude)
Excilarion frame No. 1 (pulse no. 3 position)
Excitation kame No. 1 (pulse no. 3 amplitude)
Exciration Frame No. 2 (identical to No. I )
Excitation frame No. 3 (identical to No. I)
Excitation frame No. 4 (identical to No. I)
Excitation frame No. 5 (identical to No. 1 )
Table A7-2
Table A7-3
Table A7-4
Table A7-5
Table A7-6
Table A7-7
Table A7-8
Table A7-9
Table A7-10
Table A7-11
4.10.3.1
4.10.3.2
Table A7-12
Table A7-13
Table A7-I 6
Table A7-14
Table A7-16
Table A7-14
Tablc A7-16
Table A7-15
Table A7-18. Protected partial correlation coefficient line code bits
Parcor coefficient
2 3 4 5 6 7 8 9 10
Table A7-19. Burst error detection
calculation matrix
PPPPPPPP
PPPPPPPP
PPPPPPPP
ppeeceee
bbbbbbbb
STEP UP
[h 7, 4.6) BURST ERROR
ENCODE
IWERS€ FILTER >
(W. 7, 4.7.41
-
=RIVE ERROA PULSE PCl9ITW)M
SlOWAi ENCODE
0- > -> [App. 7, 4.8.5)
WUlE
I
AWtllUOE
ENCW >
(Ppp. 7,4.6.4.1)
Part 1 Annex 10 - Aeronautical Tebcommunicaticms
I"' C'
Figure A7-2. Error detectionlcorrection precess
217
THIS PACE INTENTIONALLY LEFT BLANK
CHAPTER 5. SSR MODE S AIR-GROUND DATA LINK
[to be developed]
ANNEX 10 - VOLUME 111
CHAPTER 6. VMF AIR-GROUND DATA LINK
[to be developed]
ANNEX I0 - VOLUME 111
CHAPTER 7. SUBNETWORK INTERCONNECTION
[to be developed]
ANNEX 10 - VOLUME 111
CHAPTER 8. AFTN NETWORK
[to be developed]
ANNEX 10 - VOLUME 111
CHAPTER 9. AIRCRAFT ADDRESSING SYSTEM
[to be developed]
ANNEX 10 - VOLUME III
CHAPTER 1Q. POINT TO MULTI-POINT
COMMUNICATIONS
[to be developed]
ANNEX 10 - VOLUME III
INTERNATIONAL STANDARDS AND
IXECOMMENDED PRACTICES
PARTI 1 - VOICEC OMMUNICATIOSNY STEMS
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