ILS Flashcards
ILS provides what
Vertical guidance down glide path + Horizontal guidance along centreline (localiser)
Localiser
Provides guidance left and right to runway
VHF transmitter with 40 dedicated frequencies between 108/111.95MHz
Glide Path
Up and down guidance on approach
Transmits in the UHF/paired with VHF localiser frequency
ILS Frequency Band
VHF - 108MHz to 112MHz
Odd numbers less than 112 in the VHF band
Components of ILS
Localiser
Glide slope
DME range to indicate distance
Market beacons
ILS is identified by
3 letter Morse code
Principles of localiser
Difference of depth of modulation
Blue lobe - 150Hz
Yellow lobe - 90Hz
Modulation increases across lobe to max furthest from centreline
Ac receiver detects and measures depth of modulation in each lobe and calculates the difference.
More 90Hz than 150Hz = left of centreline
More 150Hz than 90Hz = right of the centreline
Errors associated with false localiser beams
Reversed sense side lobes cause incorrect indication of the detected modulated frequency (fly right command when already right of centre line)
Localiser coverage range
Protected ranges +- 10 degrees of runway centreline out to 25nm
+- 35 degrees out to 17nm
Localiser back course
Non precision approach on the opposite side on runway - azimuth guidance
Glide path - principles of operation
Vertical guidance by overlapping beams of UHF carrier waves
Lower (blue) - 150Hz
Upper (yellow) - 90Hz
More 150Hz signal than 90Hz = below the GP (fly up command)
More 90Hz signal than 150Hz = above the GP (flow down command)
Equal amount of each signal = DDM zero on glide path
Glide path Coverage
+- 8 degrees either side of runway centreline - 10nm
False glide path
Lower lobe is blocked by the ground/occurs above true glide path 2x
Standard 3 degree glide path = first false glide path occurs at 3 x 2 = 6 degrees
Outer Marker
Indicated the final approach fix
4-7nm from runway threshold
Lowest frequency of the three (400hz)
Blue flashing lights
2 dashes per second - - - - - - - -
Beam Bends
Slight curves which are caused by reflections of the radio wave due to obstructions. Can be followed by the navigation system of aircraft
Middle Marker
1nm from threshold
Amber
Medium frequency (1300Hz)
Dots and dashes - 3 dashes per second - . - . - . - . - . -
FM broadcast just below 108MHz can cause
Interference with localiser signal which may lead to deviation
ILS beam bends are
Slight curves caused by reflection of radio waves due to permanent obstructions. Can be followed by nav systems.
Checked by flight tests