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FINAL REPORT - Stakeholders - Ofcom

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visual) approach to the active runway. It may also be used in precision area navigation<br />

(RNAV) when coupled with the elevation and distance measuring equipment that are the<br />

remaining transmitted signals.<br />

The Azimuth and Back Azimuth signal beam shapes are both fan-shaped in a vertical<br />

plane formed along any of the antenna’s radials. As viewed by the pilot of an aircraft on<br />

final approach to the runway, the azimuth beam is swept from the right-most coverage<br />

angle to the left-most in the “To” scan, and is then returned from the left to right coverage<br />

angle in the “From” scan after a specified delay at the left-most limit. The time difference<br />

between the reception of the two scans is determined. A third signal transmitted is the<br />

elevation signal. This fan-shaped beam is transmitted from the Elevation antenna located<br />

abeam the MLS datum point. The beam originates at an angle near horizontal (minimum<br />

elevation angle), scans to the upper elevation angle limit in an upward direction (the “To”<br />

scan), and then returns (the “From” scan). The time interval between the “To” and “From”<br />

scans is measured in the receiver and based on the data transmitted from the ground<br />

(concerning site geometry and configuration) the elevation angle of the aircraft is<br />

determined.<br />

The MLS system has 200 channels, with a 1MHz channel spacing (ILS has only 40<br />

channels). Technically, this allows for a nearly unlimited number of MLS installations<br />

without interference. However, low operational need means that not all of the available<br />

channels are currently required.<br />

3.4.4 Operational Requirements<br />

3.4.4.1 General navigation requirements<br />

Introduction to RNAV and RNP<br />

RNAV (or Area Navigation) is a method which permits aircraft operation on any desired<br />

flight path within the coverage of referenced navigation aids, or within the limits of the<br />

capabilities of self-contained aids (i.e. IRS/INS), or both. The Required Navigation<br />

Performance (RNP) determines the accuracy of the RNAV system to determine the<br />

aircraft’s absolute geographical position (instead of its position relative to a navigation aid,<br />

as is the case with VOR/DME etc).<br />

The RNP for aircraft in the ECAC area is mandated to RNP 5 (i.e. the containment value<br />

is 5nm) – also known as B-RNAV (Basic area navigation). States must ensure that the<br />

navigational infrastructure provided adequately supports the prescribed RNP type in a<br />

specific area (or on a specific route).<br />

RNAV represents a fundamental change in navigation philosophy. Instead of flying<br />

to/from specific navaids, aircraft can now determine their absolute position from a variety<br />

of inputs (e.g. VOR, DME, GNSS and INS). As such, the coverage of these navaids<br />

should be tailored to ensure that at all times the aircraft can determine its position to<br />

within 5nm (or whatever the RNP value is set to). Note that not all navaids are required –<br />

whatever is provided must be sufficient to provide the required performance (and possibly<br />

include a redundant system due to the criticality of the application). As a result of this<br />

concept, the practice of ‘point-to-point’ navigation is becoming rare in civil aviation.<br />

In order to facilitate this move to RNAV, many aircraft are equipped with Multi-Mode<br />

Receivers, or MMR, which integrate L-band, VHF, UHF and C-band signals in the flight<br />

management system.<br />

EN-ROUTE NAVIGATION AID REQUIREMENTS<br />

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