T1


L. W.
Diese Lernkarten erklären Grundlagen der Funknavigation für Anfänger, darunter VOR-, NDB- und ADF-Systeme sowie deren Komponenten wie Antennen und Frequenzen. Sie beschreiben Funktionsweisen, Störungen und physikalische Phänomene wie Reflexion oder Doppler-Effekt. Ideal für Schüler, um Basiswissen für Flugnavigation oder Funktechnik zu erwerben.
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19.11.2014 / 22.03.2026

Lernkarten

 A curved MLS approach can only be performed when

DME-P is available

A Cat III ILS glidepath transmitter provides reliable guidance information down to...

the surface of the runway

In which frequency band does the Microwave Landing System (MLS) operate?

 

SHF = Super High frequency

The azimuth transmitter of a Microwave Landing System (MLS) provides a fanshaped horizontal approach zone that is usually...

+ or - 40° either side of the runway centre-line

 MLS installations notified for operation, unless otherwise stated, provide azimuth coverage of...

+ or - 40° about the nominal courseline out to a range of 20 NM

ILS is subject to false glide paths resulting from...

multiple lobes of radiation patterns in the vertical plane

Which one of the following correctly lists the major ground based components of a Microwave Landing System (MLS)?

Separate azimuth and elevation transmitters, DME facility

 Assuming a five dot display, what does each of the dots on either side of the ILS localizer cockpit display represent 

0.5 degrees

An aircraft tracking to intercept the Instrument Landing System (ILS) localiser inbound on the approach side, outside the published ILS coverage angle...

may receive false course indications

Complete the following statement. Aerodrome Surface Movement Radar operates on frequencies in the (i) .......... band employing an antenna that rotates at approximately (ii.......revolutions per minute; it is (iii) ......... possible to detect aircraft type.

(i) SHF (ii) 60 (iii) sometimes

Which of the following types of radar systems is most suited for short-range operation?

primary continuous wave

Considering a primary radar system, what kind of aerials are used?

One directional antenna both for transmitting and for receiving

 In relation to radar systems that use pulse technology, the term 'Pulse Recurrence Rate (PRR)' signifies the

number of pulses per second => km = 300'000 km/s / PRR * 2

The minimum range of a primary radar, using the pulse technique, is determined by the (i)........ ; the maximum unambiguous range by the (ii)..........

(i) pulse length (ii) pulse recurrence frequency

Which one of the following statements is correct concerning the use in primary radar of continuous wave transmissions as compared with pulse transmissions?

It eliminates the minimum target reception range (Empfangsentfernung)

ILS has ? 

LLZ (Localizer) GP (Glidepath) Marker and monitoring stations

LLZ: Frequenz? Ort? identification ?

300m behind the departure end of the ray; 108.00 - 111.975 ==> Only decimals ==> two or three letters of Morse code => A2A when morse and A9 when a combination of voice

LLZ: DDM

Difference in Depth Modulation => 2 Antennen an der Seite => Two signals are transmitted besides the carrier frequency => one 90 Hz the other 150 Hz ==> Merken wenn Aircraft nicht auf centerline ist => a difference in depth of modulation => deviation bar

LLZ:  minimas

the coverage signal: Min. 25 NM and 10 Grad to teh left and right of teh extended runways centerline

Up to a distance of 17 NM: 35 to left and right  

=> outside this range the localizer needle may be centered without on the localizer 

LLZ: full deflection by teh deviation bar?

2.5 Grad to each side ( 2450 m between LLZ: antenna and threshold)

LLZ: CDI Back-Beam Approach

150 hz modulation applies to the left hand side and the 90 Hz to the right hand side ==> Fly away from the needle

GP: Ort? Frequenz? 

1000 fet (300m) behind the threshold and 500 ft (150m) displaced from the centerline ; UHF => 328.6 MHz to 335.4 MHz => not published in the AIP O> coordinated with the published LLZ frequencies

GP: Grundprinzip and minima

a similar way, the 90 Hz modulation dominate date upper lobe while the 150 Hz modulation the lower lobe => min of 10 NM and 8 Grad to the left and right ==> In the vertical: 0.45 times to 1.75 times the nominal glide path angle

As the GP antenna is not located on teh rwy, glide path guidance is not possible all the way down to the ground or belows antenna height => Höhe ?

50 ft ==> Cat III jedoch bis zum touchdown

GP:  Full deflection of the Instrument (HSI oder CDI) by teh glide path?

+/- 0.7 degrees for a nominal GP angle of 3 degrees

Marker Bacon: was? Frequen? 

transmit a radio signal directly overhead a specific position => 75 MHz

Marker Bacon: Arten

Fan marker (FM): = >used by ILS

Zero marker: above NDB stations to fill out the cone of confusion 

3 Arten marker beacon used in combination with ILS 

OM (Outer Marker): between 4-7 Nm => 5 NM => 250 feet from either side extended rwy ==> Morse-style dashes                                       (400Hz)  = blue

MM (Middle Marker): 0.5 - 0.8 NM ahead of the rwy threshold => 250 feet from either side => morse dashes and dots (Punkte)  (1300 HZ) = amber

IN (Inner Marker): imminent arrival at teh rwy => 100 ft from eitehr side => morse dots (3000 HZ) = weight 

Grundfehler beim localizer 

selbe wie beim VOR => Bend amplitude and scalopping 

Weitere Fehler bei der ILS

Beam noise: radio beams affected by disturbance on their wys through teh atmosphere

Vehicles or other Aircrafts: signal interference by either surface vehicles or other aircrafts

Snow and Heavy Rain: a change in the diectional radio pattern of the glide slope signal

FM Broadcast Signal just below 108 MHz: => filters 

Which principle is used by localizer measurements ?

Difference in Depth of Modulation (DDM)

What happens during a localiser approach when teh aircraft deviates from the extended centerline of the approached runways towards the right 

The Difference in Depth of Modulation increases linearly from zero to 0.155 within the proportional zone

Consider teh non-approach side of an ILS installation. Which statement describes teh use of teh back bam correctly 

The back beam may be utilized for a Non-precision Approach with reversed indications

(MLS): Was ist das?

 

Microwave landing system: Satellite systems (GPS etc.) in combination withe augmentation systems are expected to replace the ILS

Microwave landing system (MLS): Grundprinzip , Frequenz 

Send a S-band from 5031 - 5091 MHZ => SHF ==> swept it across the coverage area at a fixed scan rate (To and FRO scans) => measuring the time between the received signals (hits) the airborne receiver is able to calculate its relative position

==>==> If the TO time and FRO time is teh same, teh aircraft is on the centerline 

Microwave landing system (MLS): consist aus?

an approach station, a back approach or missed approach station, an elevation 1station (GP) and an elevation 2 station (flare guidance) and a standard DME

Microwave landing system (MLS): Was ist gegenpber der ILS besser?

1. parallel, segmental and curved approaches to the rwy

2.expanded coverage

3. higher guidance accuracy

4. less sensitive to weather, obstacles

5. no interference problems (FM radio)

6. digital data link

Microwave landing system (MLS): minimas coverage 

+/- 40 degrees azimuth 0.9 - 15 Elevation

Microwave landing system (MLS): curved approach was braucht es 

to allows for segmented and curved approaches a computer (FMS) and a database are requires as well in order to compare the actual position to the programed approached trajectory == >multi Mode Receiver (MMR)

Microwave landing system (MLS): If one wants to replace an ILS with an MLS and limits the operation to the standard ILS straight in approach ==> one can manage the installation without a 

DME-P => the respective on-board indications are similar to ILS indications

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