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Technical Provisions for Mode S Services and Extended Squitter

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Appendix A A-43<br />

MB FIELD<br />

1 MSB TRANSMISSION RATE<br />

2<br />

DRAFT - Working Paper ASP TSGWP11-01 <strong>for</strong> review by the TSG during the meeting in June 2011 in Paris<br />

LSB SUBFIELD (TRS)<br />

3 ALTITUDE TYPE SUBFIELD (ATS)<br />

4<br />

5<br />

6<br />

7<br />

8<br />

9<br />

10<br />

11<br />

12<br />

13<br />

14<br />

15<br />

16<br />

17<br />

18<br />

19<br />

20<br />

21<br />

22<br />

23<br />

24<br />

25<br />

26<br />

27<br />

28<br />

29<br />

30 RESERVED<br />

31<br />

32<br />

33<br />

34<br />

35<br />

36<br />

37<br />

38<br />

39<br />

40<br />

41<br />

42<br />

43<br />

44<br />

45<br />

46<br />

47<br />

48<br />

49<br />

50<br />

51<br />

52<br />

53<br />

54<br />

55<br />

56<br />

Table A-2-7. BDS Code 0,7 — <strong>Extended</strong> squitter status<br />

PURPOSE: To provide in<strong>for</strong>mation on the capability <strong>and</strong> status<br />

of the extended squitter rate of the transponder.<br />

Transmission rate subfield (TRS) shall be coded as follows:<br />

0 = No capability to determine surface squitter rate<br />

1 = High surface squitter rate selected<br />

2 = Low surface squitter rate selected<br />

3 = Reserved<br />

Altitude type subfield (ATS) shall be coded as follows:<br />

0 = Barometric altitude<br />

1 = GNSS height (HAE)<br />

Aircraft determination of surface squitter rate:<br />

For aircraft that have the capability to automatically determine their<br />

surface squitter rate, the method used to switch between the high <strong>and</strong><br />

low transmission rates shall be as follows:<br />

a) Switching from high to low rate: Aircraft shall switch from high to low<br />

rate when the on-board navigation unit reports that the aircraft’s<br />

position has not changed more than 10 metres in any 30 second<br />

interval. The algorithm used to control the squitter rate shall save the<br />

aircraft’s position at the time that low rate is selected.<br />

b) Switching from low to high rate: Aircraft shall switch from low to high<br />

rate as soon as the aircraft’s position has changed by 10 metres or<br />

more since the low rate was selected.<br />

For transponder-based implementations, the automatically selected<br />

transmission rate shall be subject to being overridden by comm<strong>and</strong>s<br />

received from the ground control.<br />

Draft<br />

DRAFT - Working Paper ASP TSGWP11-01 <strong>for</strong> review by the TSG during the meeting in June 2011 in Paris

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