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Division Segmentation of airborne segments

United Kingdom

Original text. Later amendments are not shown.

After the segmented flight path has been derived according to the procedure described in Section 2.7.13 and the sub-segmenting described is applied, further segmentation adjustments may be necessary. These include

  • the removal of flight path points which are too close together and

  • the insertion of additional points when speed changes along segments are too long.

When adjacent points are within 10 metres of each other, and when the associated speeds and thrusts are the same, one of the points shall be eliminated.

For airborne segments where there is a significant speed change along a segment, this shall be subdivided as for the ground roll, i.e.

n seg = int 1 + V 2 − V 1 ∕ 10 (2.7.16)

where V1 and V2 are the segment start and end speeds respectively. The corresponding sub-segment parameters are calculated in a similar manner as for the takeoff ground roll, using equations (2.7.11) to (2.7.13).

Notes on Division 2.7.13

Footnotes

f1

For this purpose the total length of the ground track should always exceed that of the flight profile. This can be achieved, if necessary, by adding straight segments of suitable length to the last segment of the ground track.