Aeronautical Navigation Systems and Communication in Aircrafts

Running head: AERONAUTICAL
AERONAUTICAL
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Name of the University
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2AERONAUTICAL
Table of Contents
Part 1..........................................................................................................................................3
VOR.......................................................................................................................................3
ILS..........................................................................................................................................3
DME.......................................................................................................................................3
ADF........................................................................................................................................4
Doppler Navigation system....................................................................................................4
Inertial Navigation System.....................................................................................................4
Part 2..........................................................................................................................................5
References..................................................................................................................................6

3AERONAUTICAL
Part 1
VOR
VHF Omni directional radio range (VOR) can be considered as a type of short range
radio signal which is related to the navigation system of the aircraft. This aspect directly
enables aircraft with a receiving unit which directly determine the position of aircraft and stay
on course by means of receiving radio signals which are directly transmitted by a network of
fixed ground radio beacon. The VOR directly produces an angle between the station and the
receiver of the aircraft while the distance measuring equipment does the same for the concept
of the range (Sabatini et al. 2014).
ILS
The full form is ILS is Instrument landing system. The definition which can be
applied to the concept so that it is a precision of the runway approach aid based system. The
main composition of the system are two radio beams which are together which provides the
pilot with both the access which is horizontal as well as vertical guidance during the aspect of
landing in the ground (Zhao et al. 2017). The frequency which is related to the localizer is in
the range of 108.1-111.95 MHz and the glide slope is directly between the range of 329.15-
335.0 MHz. these are the main frequency in which the modulation aspect of the aircraft ios
basically done.
DME
The main aspect which can be related to the concept of the DME is that it is a
combined radio navigation station relating to the aircraft. The main components which are
related to the DME are two radio neocons which are placed together which are distance
measurement equipment (DME) and omnidirectional range (VOR). The main functionality