There are also excellent tools available
which are intended for studying principal effects and for training purposes
and are not intended primarily for quantitative and rigorous analysis due
to the level of theoretical methods involved. The application of these
tools for practical problems and the interpretation of these results should
be handled with great care and only within the range of the applicability.
The preferred method for the general
complex 3D-analysis is the GTD/UTD-method. It can be applied most efficiently
for the tridimensional case of the image type glideslope to optimize the
antenna geometry and to determine the monitor position and performance.
The above mentioned multilayer method can be added to take into account
the snow on the ground (dry, wet and combinations etc.) or to describe
more realistically the characteristics of buildings made of concrete.
The general numerical methods are
invariant against the system in principle. The GTD/UTD is an example which
can be applied for ILS, VOR, TACAN, MLS etc. However, the system analysis
part has to be adapted and applied to yield the decisive system parameter(s),
i.e. the
-
DDM/SDM for ILS
-
azimuth accuracy for VOR (TACAN)
-
range error for DME
-
angular error, PFE, CMN for MLS etc.
Other field parameters, e.g. field perturbations,
radar cross section, are worthless if they are not transferred uniquely
to the mentioned system parameter.
The use of numerical methods is a
powerful and cost effective technique allowing great flexibility in the
prediction of system performance but caution must be exercised to ensure
that the method used is appropriate to the application. The achieved accuracy
depends to a large extent on the validity and the adequateness of the developed
numerical model compared to the real world.
Especially the specified tolerances
with respect to the accuracy of the model must be observed very closely.
E.g., in the runway region for ILS CATIII the deviation of the system is
not to exceed a very small number (i.e. 5µA) where it is hard to
achieve an accuracy for the model that makes decisions for models definitive.
General practical experience and practical results of analog cases may
support the verification of the numerical results.
The reader is referred for further
details and for in depth publications to the open literature on numerical
methods.
Acknowledgement
The comments of Mr. Jules Hermens
(Dutch CAA, LVNL), Mr. Heinz Wipf (Swiss CAA, Swisscontrol) and Mr. Nelson
Sponheimer (FAA) are appreciated.