OpenLegislation

Division Ground track

United Kingdom

Original text. Later amendments are not shown.

A ground track, whether a backbone track or a dispersed sub-track, is defined by a series of (x,y) coordinates in the ground plane (e.g. from radar information) or by a sequence of vectoring commands describing straight segments and circular arcs (turns of defined radius r and change of heading Δξ).

For segmentation modelling, an arc is represented by a sequence of straight segments fitted to sub-arcs. Although they do not appear explicitly in the ground-track segments, the banking of aircraft during turns influences their definition. Appendix B4 explains how to calculate bank angles during a steady turn but of course these are not actually applied or removed instantaneously. How to handle the transitions between straight and turning flight, or between one turn and an immediately sequential one, is not prescribed. As a rule, the details, which are left to the user (see Section 2.7.11), are likely to have a negligible effect on the final contours; the requirement is mainly to avoid sharp discontinuities at the ends of the turn and this can be achieved simply, for example, by inserting short transition segments over which the bank angle changes linearly with distance. Only in the special case that a particular turn is likely to have a dominating effect on the final contours would it be necessary to model the dynamics of the transition more realistically, to relate bank angle to particular aircraft types and to adopt appropriate roll rates. Here it is sufficient to state that the end sub-arcs Δξtrans in any turn are dictated by bank angle change requirements. The remainder of the arc with change of heading Δξ – 2 · Δξtrans degrees is divided into nsub sub-arcs according to the equation:

nsub = int(1 + (Δξ – 2 · Δξtrans )/30)(2.7.3)

where int(x) is a function that returns the integer part of x. Then the change of heading Δξsub of each sub-arc is computed as

Δξsub = (Δξ – 2 · Δξtrans )/nsub (2.7.4)

where nsub needs to be large enough to ensure that Δξsub ≤ 30 degrees. The segmentation of an arc (excluding the terminating transition sub-segments) is illustrated in Figure 2.7.f f1.

Figure 2.7.f

Construction of flight path segments dividing turn into segments of length Ds (upper view in horizontal plane, lower view in vertical plane)

Annotations

Footnotes

f1

Defined in this simple way, the total length of the segmented path is slightly less than that of the circular path. However the consequent contour error is negligible if the angular increments are below 30°.

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.