Ohio University/FAA Flight Test Demonstration Results of the Local Area Augmentation System (LAAS)
1997
Local Area Augmentation System (LAAS) flight tests
were conducted at the William J. Hughes Technical
Center using an FAA-operated Boeing 727 aircraft. This
demonstration represents the first full-scale testing of the
proposed LAAS architecture and verifies the accuracy
and integrity monitoring fimction of the FAARTCA
LMS design.
‘fhe LAAS, as implemented for the tests, consists of three
multipath-mitigating antenna systems, six narrow-correlator
GPS C/A-code receivers, and supporting
processors. Transmission to the aircraft of the LMS
GPS differential corrections and integrity information is
accomplished using the Very-High Frequency (VHF)
navigation augmentation broadcast signal (NABS) – a
time-division, multiple-access (TDMA) broadcast signal
specifically designed for ground-to-air data
communications using frequencies in the upper VHF
Omni-Range (VOR) band.
In the aircratl, the NABS-transmitted ditTerential
corrections are combined with GPS data from two
narrow-correlator C/A-code receivers to produce a
redundant aircraft position. The aircraft position is
derived from carrier-smoothed code measurements.
The results of the flight tests demonstrate the feasibility of
. key components of the LAAS architecture, including the
multipath-lirniting antenna system, the implementation of
the integrity equations, and the use of the VHF data
broadcast. Data processed from 45 approaches results in
differential GPS sensor accuracies of 0.46 meters (957.)
vertical and 0.22 meters (950A)cross-track on a 3-degree
glidepath at a height of 100 feet above the ground.
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