If you wish to contribute or participate in the discussions about articles you are invited to join SKYbrary as a registered user


Work in progress

Difference between revisions of "Localiser Performance with Vertical Guidance (LPV)"

From SKYbrary Wiki

(Related Articles)
Line 41: Line 41:
*[[Wide Area Augmentation System (WAAS)]]
*[[Wide Area Augmentation System (WAAS)]]
*[[European Geostationary Navigation Overlay Service (EGNOS)]]
*[[European Geostationary Navigation Overlay Service (EGNOS)]]
==Further Reading==

Revision as of 13:17, 22 October 2019

Article Information
Category: General General
Content source: SKYbrary About SKYbrary
Content control: SKYbrary SKYbrary
Ambox content.png
The present article is under construction.
Reader enquiries are welcome, contact the editor: editor@skybrary.aero.
Ambox content.png


Localizer Performance with Vertical Guidance


Work in progress:Localiser Performance with Vertical Guidance (LPV) is defined as an Approach with Vertical Guidance (APV); that is, an instrument approach based on a navigation system that is not required to meet the precision approach standards of ICAO Annex 10 but that provides both course and glidepath deviation information.

The lateral guidance is equivalent to a localizer, and the protected area is considerably smaller than that provided for current LNAV or LNAV/VNAV approaches. Aircraft can fly to LPV minimums with a statement in the Aircraft Flight Manual (AFM) that the installed equipment supports LPV approaches.


Localiser Performance with Vertical Guidance (LPV) is a subset of Area Navigation (RNAV) Approach minima that are available at some locations. Approaches to LPV minima have characteristics which are very similar to an Instrument Landing System (ILS) approach. The fundamental difference between the two is the source of the guidance signals. Whilst an ILS is a ground based approach, necessitating the associated transmitters and antennae for each runway, the source for RNAV LPV guidance is the space based Global Navigation Satellite System (GNSS) which can be used to simultaneously provide the guidance for multiple approaches at multiple locations.

RNAV GNSS approaches that can be conducted down to LPV minima are characterised by a coded Final Approach Segment (FAS) data block. The FAS is defined laterally by the Flight Path Alignment Point (FPAP) and Landing Threshold Point/Fictitious Threshold Point (LTP/FTP). It is defined vertically by the Threshold Crossing Height (TCH) and Glide Path Angle (GPA). The FAS of an LPV approach may be intercepted by an approach transition, such as Precision-Area Navigation (P-RNAV), the initial and intermediate segments of an RNP Approach, or through radar vectoring to intercept the extended FAS.

To provide the necessary accuracy to conduct an approach to LPV minima, the GNSS signal must be refined by a Satellite Based Augmentation System (SBAS) system, be it the Wide Area Augmentation System (WAAS), the European Geostationary Navigation Overlay Service (EGNOS) or another space based augmentation system. These extremely accurate augmentation systems can provide the required lateral and vertical guidance down to a decision altitude (DA), just like an ILS. In the same fashion as an ILS, the angular guidance of an LPV approach becomes narrower and more sensitive as the aircraft approaches the runway. To enable use of LPV minima, the aircraft must be fitted with both an LPV capable Flight Management System (FMS) and a compatible SBAS receiver.


RNAV approaches, inclusive of those with LPV minima, have been designed and certified for use at numerous European, American and Canadian airports. In many cases, the newly implemented approaches allow for the equivalent of Category I ILS capability at locations which previously could not support, or justify the cost of, an ILS installation. Additional approaches are being designed and added year over year. As of June 2019, there were almost 4000 RNAV approaches with LPV minima within the United States, of which more than 1100 serve airports which previously did not have an ILS capability.

Approach Execution


LPV minima take advantage of the high accuracy guidance and increased integrity provided by SBAS (WAAS, EGNOS etc). The SBAS generated angular guidance allows the use of the same approach design criteria that is used for ILS approaches. LPV minima may have a decision altitude (DA) as low as 200 feet height above touchdown zone elevation with associated visibility minimums as low as 1/2 mile, when the terrain and airport infrastructure support the lowest allowable minima.

Related Articles

Further Reading