21.03.2013 Views

Aircraft Operations. Volume II - Construction of Visual and Instrument ...

Aircraft Operations. Volume II - Construction of Visual and Instrument ...

Aircraft Operations. Volume II - Construction of Visual and Instrument ...

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

Chapter 1<br />

MINIMUM LENGTH OF A SEGMENT LIMITED BY<br />

TWO TURNING WAYPOINTS<br />

1.1 GENERAL<br />

1.1.1 To prevent turning waypoints being placed so close that RNAV systems are forced to bypass them, a<br />

minimum distance between successive turning waypoints must be taken into account. Two types <strong>of</strong> waypoints are<br />

considered:<br />

a) fly-by waypoint; <strong>and</strong><br />

b) flyover waypoint.<br />

1.1.2 Four sequences are possible for a segment limited by two waypoints:<br />

a) two fly-by waypoints;<br />

b) fly-by waypoint, then flyover waypoint;<br />

c) two flyover waypoints; <strong>and</strong><br />

d) flyover waypoint, then fly-by waypoint.<br />

In addition, the particular case <strong>of</strong> the segment “DER — first waypoint” must also be considered.<br />

1.1.3 The following method is based on theoretical studies combined with the results <strong>of</strong> simulations. Some<br />

differences may exist between RNAV systems; algorithms used by these systems are complex. For these reasons,<br />

simplifications were made when establishing theoretical formulae.<br />

1.1.4 The aim <strong>of</strong> the method is not to determine a protection area, but to determine a minimum distance between<br />

two waypoints on a nominal trajectory. For this reason, wind effect <strong>and</strong> waypoint tolerances are not taken into account<br />

in the theoretical calculations. When it is necessary, greater values may be chosen.<br />

1.2 DETERMINATION OF THE MINIMUM LENGTH OF THE RNAV SEGMENT<br />

1.2.1 General<br />

For each waypoint a minimum stabilization distance is determined. This is the distance between the waypoint <strong>and</strong> the<br />

point where the trajectory joins tangentially with the nominal track (Figure <strong>II</strong>I-2-1-1). For successive waypoints, the<br />

minimum distance between them is the sum <strong>of</strong> both minimum stabilization distances. The tables in this chapter show<br />

minimum stabilization distances for various values <strong>of</strong> true airspeed <strong>and</strong> course change (at the waypoint).<br />

<strong>II</strong>I-2-1-1 23/11/06

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!