- •Textbook Series
- •Contents
- •1 Properties of Radio Waves
- •Introduction
- •The Radio Navigation Syllabus
- •Electromagnetic (EM) Radiation
- •Polarization
- •Radio Waves
- •Wavelength
- •Frequency Bands
- •Phase Comparison
- •Practice Frequency (
- •Answers to Practice Frequency (
- •Questions
- •Answers
- •2 Radio Propagation Theory
- •Introduction
- •Factors Affecting Propagation
- •Propagation Paths
- •Non-ionospheric Propagation
- •Ionospheric Propagation
- •Sky Wave
- •HF Communications
- •Propagation Summary
- •Super-refraction
- •Sub-refraction
- •Questions
- •Answers
- •3 Modulation
- •Introduction
- •Keyed Modulation
- •Amplitude Modulation (AM)
- •Single Sideband (SSB)
- •Frequency Modulation (FM)
- •Phase Modulation
- •Pulse Modulation
- •Emission Designators
- •Questions
- •Answers
- •4 Antennae
- •Introduction
- •Basic Principles
- •Aerial Feeders
- •Polar Diagrams
- •Directivity
- •Radar Aerials
- •Modern Radar Antennae
- •Questions
- •Answers
- •5 Doppler Radar Systems
- •Introduction
- •The Doppler Principle
- •Airborne Doppler
- •Janus Array System
- •Doppler Operation
- •Doppler Navigation Systems
- •Questions
- •Answers
- •6 VHF Direction Finder (VDF)
- •Introduction
- •Procedures
- •Principle of Operation
- •Range of VDF
- •Factors Affecting Accuracy
- •Determination of Position
- •VDF Summary
- •Questions
- •Answers
- •7 Automatic Direction Finder (ADF)
- •Introduction
- •Non-directional Beacon (NDB)
- •Principle of Operation
- •Frequencies and Types of NDB
- •Aircraft Equipment
- •Emission Characteristics and Beat Frequency Oscillator (BFO)
- •Presentation of Information
- •Uses of the Non-directional Beacon
- •Plotting ADF Bearings
- •Track Maintenance Using the RBI
- •Homing
- •Tracking Inbound
- •Tracking Outbound
- •Drift Assessment and Regaining Inbound Track
- •Drift Assessment and Outbound Track Maintenance
- •Holding
- •Runway Instrument Approach Procedures
- •Factors Affecting ADF Accuracy
- •Factors Affecting ADF Range
- •Accuracy
- •ADF Summary
- •Questions
- •Answers
- •8 VHF Omni-directional Range (VOR)
- •Introduction
- •The Principle of Operation
- •Terminology
- •Transmission Details
- •Identification
- •Monitoring
- •Types of VOR
- •The Factors Affecting Operational Range of VOR
- •Factors Affecting VOR Beacon Accuracy
- •The Cone of Ambiguity
- •Doppler VOR (DVOR)
- •VOR Airborne Equipment
- •VOR Deviation Indicator
- •Radio Magnetic Indicator (RMI)
- •Questions
- •In-flight Procedures
- •VOR Summary
- •Questions
- •Annex A
- •Annex B
- •Annex C
- •Answers
- •Answers to Page 128
- •9 Instrument Landing System (ILS)
- •Introduction
- •ILS Components
- •ILS Frequencies
- •DME Paired with ILS Channels
- •ILS Identification
- •Marker Beacons
- •Ground Monitoring of ILS Transmissions
- •ILS Coverage
- •ILS Principle of Operation
- •ILS Presentation and Interpretation
- •ILS Categories (ICAO)
- •Errors and Accuracy
- •Factors Affecting Range and Accuracy
- •ILS Approach Chart
- •ILS Calculations
- •ILS Summary
- •Questions
- •Answers
- •10 Microwave Landing System (MLS)
- •Introduction
- •ILS Disadvantages
- •The MLS System
- •Principle of Operation
- •Airborne Equipment
- •Question
- •Answer
- •11 Radar Principles
- •Introduction
- •Types of Pulsed Radars
- •Radar Applications
- •Radar Frequencies
- •Pulse Technique
- •Theoretical Maximum Range
- •Primary Radars
- •The Range of Primary Radar
- •Radar Measurements
- •Radar Resolution
- •Moving Target Indication (MTI)
- •Radar Antennae
- •Questions
- •Answers
- •12 Ground Radar
- •Introduction
- •Area Surveillance Radars (ASR)
- •Terminal Surveillance Area Radars
- •Aerodrome Surveillance Approach Radars
- •Airport Surface Movement Radar (ASMR)
- •Questions
- •Answers
- •13 Airborne Weather Radar
- •Introduction
- •Component Parts
- •AWR Functions
- •Principle of Operation
- •Weather Depiction
- •Control Unit
- •Function Switch
- •Mapping Operation
- •Pre-flight Checks
- •Weather Operation
- •Colour AWR Controls
- •AWR Summary
- •Questions
- •Answers
- •14 Secondary Surveillance Radar (SSR)
- •Introduction
- •Advantages of SSR
- •SSR Display
- •SSR Frequencies and Transmissions
- •Modes
- •Mode C
- •SSR Operating Procedure
- •Special Codes
- •Disadvantages of SSR
- •Mode S
- •Pulses
- •Benefits of Mode S
- •Communication Protocols
- •Levels of Mode S Transponders
- •Downlink Aircraft Parameters (DAPS)
- •Future Expansion of Mode S Surveillance Services
- •SSR Summary
- •Questions
- •Answers
- •15 Distance Measuring Equipment (DME)
- •Introduction
- •Frequencies
- •Uses of DME
- •Principle of Operation
- •Twin Pulses
- •Range Search
- •Beacon Saturation
- •Station Identification
- •VOR/DME Frequency Pairing
- •DME Range Measurement for ILS
- •Range and Coverage
- •Accuracy
- •DME Summary
- •Questions
- •Answers
- •16 Area Navigation Systems (RNAV)
- •Introduction
- •Benefits of RNAV
- •Types and Levels of RNAV
- •A Simple 2D RNAV System
- •Operation of a Simple 2D RNAV System
- •Principle of Operation of a Simple 2D RNAV System
- •Limitations and Accuracy of Simple RNAV Systems
- •Level 4 RNAV Systems
- •Requirements for a 4D RNAV System
- •Control and Display Unit (CDU)
- •Climb
- •Cruise
- •Descent
- •Kalman Filtering
- •Questions
- •Appendix A
- •Answers
- •17 Electronic Flight Information System (EFIS)
- •Introduction
- •EHSI Controller
- •Full Rose VOR Mode
- •Expanded ILS Mode
- •Full Rose ILS Mode
- •Map Mode
- •Plan Mode
- •EHSI Colour Coding
- •EHSI Symbology
- •Questions
- •Appendix A
- •Answers
- •18 Global Navigation Satellite System (GNSS)
- •Introduction
- •Satellite Orbits
- •Position Reference System
- •The GPS Segments
- •The Space Segment
- •The Control Segment
- •The User Segment
- •Principle Of Operation
- •GPS Errors
- •System Accuracy
- •Integrity Monitoring
- •Differential GPS (DGPS)
- •Combined GPS and GLONASS Systems
- •Questions
- •Answers
- •19 Revision Questions
- •Questions
- •Answers
- •Specimen Examination Paper
- •Appendix A
- •Answers to Specimen Examination Paper
- •Explanation of Selected Questions
- •20 Index
VHF Direction Finder (VDF) 6
Principle of Operation
The only equipment required to obtain a VDF bearing is a VHF radio; some specialist equipment is required on the ground: a suitable aerial and a display.
A VHF voice communications radio produces a vertically polarized signal; therefore, the ground antenna is vertically polarized and has an array of vertical elements arranged in a circle. See
Figure 6.2.
VHF Direction FInder (VDF) 6
Figure 6.2: Obtaining a VDF Bearing
The equipment resolves the bearing from transmissions received at each element within the array. The bearing is then displayed on the display. The bearing can be displayed relative to either True or Magnetic North (at the station).
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6 VHF Direction Finder (VDF)
(VDF) Finder Direction VHF 6
Range of VDF
•As VDF utilizes the VHF Band (or UHF as required) the range will obey the line of sight formula: the higher the transmitters the greater the reception range
Line of sight Range (MTR) = 1.23 × (√hTX + √hRX)
•Intervening high ground will limit range, especially for low flying aircraft in hilly terrain.
•The power of airborne and ground transmitters will limit ranges.
•Gradients of temperature and humidity can give greater than line of sight range.
Factors Affecting Accuracy
•Propagation error and site error caused by the aircraft’s transmissions being reflected from terrain as they travel to the site, or being reflected from buildings at the site.
•Aircraft attitude: the VDF System and VHF Communications are vertically polarized; therefore, best reception and results will be obtained when the aircraft flies straight and level.
•Poor accuracy is likely in the overhead of a VDF receiver, particularly with the latest Doppler systems. The reception of both Direct Wave and Ground Reflected Wave can cause signal fading or loss; the phenomenon is usually short-lived. Together with other multi path signals this gives rise to bearing errors.
•Synchronous transmissions by two or more aircraft will cause momentary errors in bearings.
Determination of Position
If there are sufficient ground stations, linked to an ATCC, the aircraft’s position can be fixed using auto-triangulation and the position transmitted to the pilot. This facility may be available to Distress and Diversion Cells, but can not be guaranteed.
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VHF Direction Finder (VDF) |
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VDF Summary |
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Bearings: |
QDM |
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Mag TO Station |
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QDR |
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Mag FROM Station |
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QUJ |
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True TO Station |
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QTE |
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True FROM Station |
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Uses: |
Track Check |
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Position Line |
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Homing |
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Let-downs |
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Class: |
A = ± 2° |
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FInder |
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B = ± 5° |
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C = ± 10° |
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Direction |
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D = > 10° |
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Principle: |
Ground Equipment – Direction Finding Aerial |
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VHF |
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CRT Display |
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Range: |
Line of Sight |
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Power of Transmitters |
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Intervening High Ground |
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Accuracy: |
Propagation Error |
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Site Error |
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Overhead |
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Position Service: |
Position Fixing by Auto-triangulation |
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Figure 6.3 VDF Summary
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6 Questions
Questions 6
Questions
1.An aircraft has to communicate with a VHF station at a range of 300 NM, if the ground station is situated 2500 ft AMSL which of the following is the lowest altitude at which contact is likely to be made?
a.190 ft
b.1 378 ft
c.36 100 ft
d.84 100 ft
2.Class ‘B’ VHF DF bearings are accurate to within:
a.± 1°
b.± 5°
c.± 2°
d.± 10°
3.A VDF QDM given without an accuracy classification may be assumed to be accurate to within:
a.2 degrees
b.5 degrees
c.7.5 degrees
d.10 degrees
4.An aircraft at altitude 9000 ft wishes to communicate with a VHF/DF station that is situated at 400 ft AMSL. What is the maximum range at which contact is likely to be made?
a.115 NM
b.400 NM
c.143 NM
d.63.5 NM
5.An aircraft is passed a true bearing from a VDF station of 353°. If variation is 8°E and the bearing is classified as ‘B’ then the:
a.QDM is 345° ± 5°
b.QDR is 345° ± 2°
c.QTE is 353° ± 5°
d.QUJ is 353° ± 2°
6.An aircraft at 19 000 ft wishes to communicate with a VDF station at 1400 ft AMSL. What is the maximum range at which contact is likely ?
a.175 NM
b.400.0 NM
c.62.5 NM
d.219 NM
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Questions 6
Questions 6
81