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GBAS Messages

A GBAS communicates with aircraft using a standardised set of messages broadcast over the VDB link. These GBAS messages carry the corrections, integrity information and approach data required for GLS operations.

GBAS messages are structured and numbered Message Types (MT), each serving a specific function. Together, they provide:

  • Differential corrections for GNSS signals

  • Integrity and protection information

  • Definitions of GLS approaches and reference paths

  • System status and configuration data

While implementations and standards can differ slightly, the commonly referenced message types include:

  • MT1 – Pseudorange Corrections - 100s smoothed

  • MT2 – Integrity and Protection Data

  • MT4 – Approach Geometry / Final Approach Segment Data

  • MT11 – Pseudorange Corrections – 30s smoothed

Additional message types support extended services, multiple constellations, dual-frequency operation and future GAST levels.

MT1 – Pseudorange Corrections: 100s smoothed

Purpose
Message Type 1 (MT1) provides the core differential corrections that allow an aircraft to remove most of the common-mode GNSS errors seen at the airport.

Key Characteristics

  • Contains pseudorange corrections for the satellites in view and supported by the GBAS installation.

  • Corrections are derived from the ground reference receiver network and represent localised adjustments to satellite ranging signals.

  • Typically includes:

    • Satellite identifiers (e.g. PRN/SV ID)

    • Correction values and associated quality indicators

    • Time tags linking corrections to GNSS time

Airborne Use

  • The GBAS-capable receiver applies MT1 corrections to smoothed GNSS measurements.

  • This reduces errors due to satellite clock and ephemeris, as well as most local atmospheric effects within the coverage area.

  • Corrected measurements form the basis for the precision position solution used in GLS approaches.

MT2 – Integrity, Protection and System Parameters

Purpose
Message Type 2 (MT2) provides integrity and protection-related information and key system parameters needed for safe use of GBAS corrections.

Key Characteristics

  • Contains parameters that define:

    • Integrity bounds and protection-level components

    • Allocation of error budgets, including residual ionospheric and tropospheric effects

    • Validity intervals and conditions for using the broadcast corrections

  • May include:

    • Ground system configuration information

    • Indicators of which satellites are approved or excluded for use

    • Parameters supporting airborne computation of Vertical and Lateral Protection Levels (VPL/LPL)

Airborne Use

  • GLS receivers use MT2 data to:

    • Determine which satellites are eligible for use in the position solution.

    • Compute protection levels consistent with the declared GAST and minima.

    • Detect conditions in which the GBAS service is not valid (e.g. flagged anomalies).

In combination with MT1, MT2 enables the receiver to form a corrected and integrity-bounded solution suitable for precision approach.

MT4 – Final Approach Segment and Approach Path Data

Purpose
Message Type 4 (MT4) defines the approach path geometry and associated data for a GLS procedure, effectively describing the virtual localiser and glideslope that the aircraft will follow.

Key Characteristics

  • Contains Final Approach Segment (FAS) data for one or more GLS approaches served by the GBAS installation.

  • Typically encodes:

    • Runway and approach identifiers / reference path identifiers

    • Touchdown and threshold coordinates and elevations

    • Final approach course (localiser-equivalent) and glide path angle

    • Lateral and vertical path definitions, including any offsets

    • Additional parameters such as reference datum, path width and limits

Airborne Use

  • The receiver selects the appropriate GLS approach using identifiers that match the published procedure.

  • MT4 data allow the airborne system to:

    • Generate deviation signals equivalent to ILS localiser and glideslope.

    • Align the guidance with the physical runway and obstacle clearance surfaces.

  • Flight guidance systems and, where available, autoland systems use this data to fly the precision approach down to the authorized minima.

MT11 – Pseudorange Corrections: 30s smoothed

Purpose
Message Type 11 (MT11) contains differential corrections derived from carrier smoothed pseudoranges using a time constant of 30 seconds. MT11 also includes alternative parameters for integrity bounding and for optimal weighting of measurements.

Key Characteristics

  • The use of a shorter time constant reduces the differential error resulting from ionospheric activity.

  • Supports enhanced integrity monitoring for higher GAST levels (e.g. CAT II/III services) where ionospheric and other spatial effects become more critical.

Airborne Use

  • Receivers use MT11 data in combination with MT1/MT2 to:

    • Adjust protection levels and integrity calculations for spatially dependent effects.

    • Determine whether specific approach segments or geometries remain within acceptable risk bounds.

  • This allows GBAS to support lower minima and more demanding operations without excessive conservatism in protection levels.