Prepared for the ICAO AWOG (Status:
February 8, 1999)
by Dr.-Ing G. Greving, NAVCOM
Consult, Marbach, Germany
The increasing air traffic and the
lack of space for new buildings on most of the modern international airports
are serious threats for ILS-operation. Because of this, more and larger
buildings are established on the airport and relatively close to the runways.
This is especially threatening for the increasing demand for ILS CATIII
operation where the specification for the DDM-guidance parameter is most
stringent at the runway for the rollout guidance of aircraft.
ICAO Annex 10 is proposing in the
Attachment C that for every major construction activity on the airport,
a theoretical analysis and a numerical simulation should be performed.
This is to decide in advance whether the intended building is acceptable
for the assigned operational category and thus be able to sustain the current
performance or protect a future need.
The total ILS consists of a number
of system components, namely, the hardware ground equipment (transmitters,
antennas, monitors), the airborne equipment (antennas, receivers, signal
processing), and last not least, the associated environment, where the
wave propagation and the multipath generation takes place which eventually
determine the signal in space. The safeguarding of the ILS is achieved
by protection zones on the airport, i.e. the critical and sensitive areas,
and by the less obvious building restriction areas, which are much larger
than the protection zones covering areas outside the critical and sensitive
areas and extend often outside the airport. However, the experienced ILS-engineer
knows that extremely large buildings and certain assemblies of taxiing
aircraft will threaten the ILS-specs even for the most advanced systems.
This threat has to be minimized to the extent possible for safety purposes.
One means to aid this protection is the application of advanced numerical
methods together with the necessary expertise.
The whole ILS as defined above constitutes
a tremendous electromagnetic problem. It is electrically very large, i.e.
the dimensions in question are very large compared to the wavelength of
about 3m for the localizer and about 1m for the glideslope subsystem. In
addition, the problem is tridimensional from the very beginning and the
use of two-dimensional approximation is restricted to simple cases if at
all. By this, the number of possibly applicable numerical methods is limited.
The driving parameters are the required computer storage and the computer
time which must both be reasonable. It is desirable that the problems can
be solved with a modern workstation for most cases.