Skip to main content

ILS- Instrument Landing System

 Introduction to ILS

ILS is a ground based radio navigation system that helps in approach guidance in the inboard side of the aircraft. So it a procedure adopted by manny airports around the world to guide the aircraft to land safely even in harse weather conditions. It can be immagined like the rail guides that we find in airports during boarding. What this basically does is guides you throught the way.


Terminologies relevant to ILS

Before starting with the topic we need to understand some of the terminologies, one being the meterological conditions. So an aircraft approach in IMC ( Instument Meterological Conditions) or VMC (Visual Meterological Conditions) means the situation of weather condition that demands certain procedure. If the situation is IMC then we say the approach in IMC and if it is VMC then we say the approach in VMC. 

Now lets move on to next terminology .i.e. VFR and IFR. these are the set of rules that need to followed according the MC. If the Approac is in IMC then IFR should be followed and if the approach is in VMC then VFR should be followed. 

However what does this actually mean?

VFR- Visual Flight Rules

IFR- Instrument Flight Rules.


So there are a different set of rules for different procedures. If the weather is clear and visibility is high then VFR can be used i.e. relying more on the visuals of the Pilots and less on the instrument. However in the IFR rules pilots land with heavy use of  ILS.

So how do we differentiate VFR and IFR?

Here we need to understand 2 important units- visibility range and the ceiling. 

Visibility range is the farthest distance that is visible to the nacked eye. and ceiling is the altitude of the aircraft from the ground at the time of approach. 


VFR- visibility more than 5 miles. and AGL 3000 ft

Marginal VFR - visibility between 3 to 5 miles and AGL 1000 to 3000 ft

ILR- visibility between 1 to 3 miles and AGL 500 to 1000ft

low ILR- visibility lower than 1 mile and AGL lower than 500 ft.


Different guidance system in ILS

Lateral guidance: VHF

A localizer at the end/ beyond the end of the run way provides the lateral guidance during the approach. This is a set of directional antenna that focus their radio signals along the run way to the inbound. And if we have a overview of an airport with such system then we could see something like in this figure below. The antenas produce a field with the respective frequencies - 90 and 150 Hz. As the aircraft arrives near the airport these frequencies are used by the ILS reciever and displayed as a dimond in the ILS device in the aircraft.



vertical guidance-UHF now vertical axis - glideslope

A glideslope antenna at the threashold of the runway gives a similar directional signal in the vertical direction as the localizer in horizontal direction. and this is perpendicular to the touch down point. This also produces an area of 90 and 150 Hz. and the ILS uses a similar displace indication of dimond but in the vertical axis.


Marker Beacon:
as the aircraft takes the approach the aircraft flies through different marker beacons.
outer, middle and inner marker beacons. each using a DME to let the aircraft know its position from the runway threshold. 


What are necessary for an ILS?
a reciever in the cockpit with a display called ILS.
an approach chart with important information like frequency (Moars code), ILS inbound course and glideslope angle and final approach point. 

the frequency also contains information about the built in DME if the ILS in the airport has a DME then the code will start with a D. 




Comments

Popular posts from this blog

ACARS (Aircraft Communications Addressing and Reporting System)

ACARS This is a neat way used to bypass the intentional or unintentional human error on  reporting flight information during or after flight . Before 1978 AD, this information was given via, voice logs, where captain verbally records the phase of flight and time. This brought human error in the data reporting and was extra work to the pilots.  What ACARS does is acts as a reporting machine which reports flight information in different phases of flight to the Ground team. Initially ARINC developed this method for just 4 messages per flight, but now it has turned into a robust means of data link between not just aircraft and ground station but also between aircraft.  ACARS (Aircraft Communications Addressing and Reporting System) is a data communications system used for air-ground communication between an aircraft and their own operations centers, air traffic control, and national aviation authorities. ACARS can be used anywhere in the world by connecting to a global ne...

ATA numbering system

 An aircarft has a lot of parts, manufacturing them is one thing maintaining them is some other level challange. Thus to describe what needs to be done for what part requires a lot of documentation.  The easy way engineers have come up is to name each section of the aircraft as different title numbers.  ATA- Air Traffic association. It was created by people in ATA so called ATA chapters.  with 100 chapters ATA  So when some one says ATA chapter 72 it will always mean engine. ATA 27 flight controls ATA 32 landing gear ATA 72 is engine  and so on If we go even deeper. ATA 72-00-01 is fan module ATA 72-00-02 is core module ATA 72-00-03 is HPT Module ATA 72-00-04 is LPT module ATA 72-00-05 is AGB module and so on

PT6A-27

General Engine specification Blog1. It is a turboprop engine- free turbine . This is an engine used in airplanes like DHC-6 Twin Otter 300  Harbin Y-12 Beechcraft This a Pratt and Whitney Canada Engine. One of the most famous and successful company to produce turboprop engine. Compressor  It consist of 3 stage axial compressor and 1 stage centrifugal flow compressor. Combustion  Annular reverse flow (right to left according to diagram above) combustion with 14 simplex burner (Glow plugs) Turbine 1 stage free power turbine and 1 sage gas generator power turbine.(Left to right according to diagram above) Other specs: Fuel type: aviation kerosine Overall pressure ratio- 6.3:1 Air mass flow: 5.3 lb/s Power to weight ration: 2.14 hp/lb