- •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
Questions 8
8 Questions
Questions
1.Using the CDI shown, what is the aircraft’s QDR?
Figure 8.19
2.Using the CDI shown, what is the aircraft’s QDM?
Figure 8.20
3.Using the HSI shown, what is the aircraft’s QDR?
Figure 8.21
4.Using the HSI shown, what is the aircraft’s QDM?
Figure 8.22
128
VHF Omni-directional Range (VOR) 8
In-flight Procedures
Typical uses of VOR by an aircraft equipped with both CDI-type deviation indicator and an RMI are illustrated in Figure 8.23.
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Figure 8.23 In-flight Procedures |
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Radial Interceptions
In Figure 8.23 the aircraft is shown intercepting the 280° radial by flying a heading of about 045°(M), commencing the turn shortly before making good the radial so as not to over-shoot it.
A heading of 090°(M) is selected to allow for starboard drift inbound. So the turn is through 45° taking about 15 seconds. Arrival at the 277 radial should be announced by the Left/Right indicator showing about 1.5 dots ‘fly left’ and the RMI needle pointing a QDM of 097° at which point he would turn onto 090°(M).
InboundTrack-keeping
Having intercepted the inbound radial, the pilot maintains his heading (of 090°(M) in the Figure 8.23 example) and watches the Left/Right needle. Suppose the needle shows a progressively increasing displacement left; then the aircraft is moving to the right of the desired inbound track. The drift allowance is insufficient and a heading of 085° would perhaps be more suitable. The pilot would probably alter heading 30° port on to 060°(M) until the needle centred, indicating the aircraft to be back on track, before trying the new heading of 085°(M) and again watching the needle.
129
8 VHF Omni-directional Range (VOR)
(VOR) Range directional-Omni VHF 8
Further alterations of heading may be necessary before the aircraft is settled down on a good inbound heading with the needle reasonably steady in the central position. It is worth visualizing how the RMI would behave during the homing just described.
After the interception, the heading of 090° would show against the heading index, the RMI needle indicating 100° (the required QDM to the VOR).
Station Passage
Overhead a VOR there is a ‘cone (or zone) of confusion’ with a vertical angle of about 60° to 80° (ICAO minimum is 40°). This leads to indeterminate indications over the beacon which at high level extend over a considerable area, for instance out to about 4 NM radius at 30 000 ft.
On the VOR/ILS indicator, the needle swings between hard left and hard right, the OFF flag may appear temporarily, and the TO/FROM indicator changes to FROM. The RMI needle fluctuates and then rotates through 180° to indicate the QDM back to the beacon. At low altitude these station passage indications are rapid; at high altitude they are slow.
Outbound Flight
The aircraft is shown outbound on the 150 radial on the right-hand side of Figure 8.23. The indications are ideal, the TO/FROM flag showing ‘FROM’, and the centralized L/R needle showing the aircraft to be on the selected track of 150°. The information on the deviation indicator is confirmed by the RMI needle showing a QDM of 330 back to the beacon.
If these indications were to change, showing a track error developing, the pilot would normally make a firm heading alteration (typically 30°) to regain track before steering a revised outbound heading appropriate to his revised assessment of drift.
130
VHF Omni-directional Range (VOR) 8
Airfield Approach
VHF Omni-directional Range (VOR) 8
Figure 8.24 Example of a VOR DME approach pattern
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