- •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
Radar Principles 11
Radar Frequencies
Radar systems are in the VHF and above frequency bands because:
•these frequencies are free from external noise/static and ionospheric scatter.
•the shorter wavelengths produce narrow, efficient beams for target discrimination and bearing measurement.
•the shorter wavelengths can produce shorter pulses.
•efficient reflection from an object depends upon its size in relation to the wavelength; shorter wavelengths are reflected more efficiently.
Pulse Technique
Primary and secondary radar systems use the pulse technique which is the transmission of radio energy in very short bursts. Each burst of energy is in a pulse form of a predetermined shape. The duration of the pulse is equal to the pulse length or width. Although a pulse is of short width (time) it can contain many cycles.
+ |
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0 |
TIME |
- |
PULSE |
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WIDTH |
+ |
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0 |
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TIME |
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PULSE |
PULSE RECURRENCE INTERVAL(PRI) |
RECURRENCE |
or |
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PULSE RECURRENCE PERIOD(PRP) |
Figure 11.2 Pulse technique
Pulse Recurrence Interval (PRI) is the time interval between two pulses.
Pulse Recurrence Frequency (PRF) is the number of pulses transmitted in one second (pps). Example. If the PRF is 250 pps what is the PRI of the transmission?
PRI = 1 / 250 s
PRI = 1 000 000 / 250 µs = 4000 µs
Radar Principles 11
185
11 Radar Principles
Distance Measurement - Echo Principle
Principles Radar 11
Figure 11.3
The distance to an object is found by timing the interval between the instant of the pulse’s transmission and its return as an echo; this is shown in Figure 11.3.
For example, if the echo (the time between transmission and reception) is 500 µs then:
Distance |
= |
300 000 000 |
× |
500 |
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m |
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1 000 000 |
× 2 |
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= |
75 000 m |
= |
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75 km |
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or |
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Distance |
= |
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162 000 × 500 |
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1 000 000 × 2 |
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= |
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40.5 NM |
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(c = 300 000 000 m/s or 162 000 NM/s)
Other methods of calculating the range are:
Range = |
500 × 300 |
= |
75 km |
Range = |
500 × 300 |
= |
40.5 NM |
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2 |
2 |
× 1852 |
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A radar mile (one NM out and back) = 12.36 µs.
500
Range = 12.36 = 40.5 NM
186
Radar Principles
Theoretical Maximum Range
Relationship to PRF
Maximum theoretical range is determined by the PRF i.e. the number of pulses transmitted in one second (pps) Each pulse must be allowed to travel to the most distant object planned before the next pulse is transmitted; to do otherwise makes it impossible to relate a particular echo to a particular pulse. The maximum range is therefore related to the PRF such that the greater the range required, the lower the PRF used.
Examples
1.We wish a radar to measure a range of up to 187 km. What should the PRF (PRR) be?
2.What is the maximum PRR for a radar required to measure up to 200 NM?
3.Maximum range for a radar is to be 170 km. What is the maximum PRR?
4.An AWR has a 400 pps PRR. Calculate the maximum range in nautical miles for this equipment.
Answers
1.The pulse must travel 374 km (2 × 187) before the next pulse transmission.
The time for the journey, T = D/S |
= |
374 000/300 000 000 seconds |
|
= |
0.0012466 s = 1246 µs |
i.e. PRI |
= |
1246 µs. |
Thus the second pulse can only leave 1246 µs after the first.
PRF (pps) = 1/ PRI = 1/ 1246 µs = 1 000 000 / 1246 = 802 pps
Alternately we can say that PRF = 300 000 000 / 374 000 = 802 pps
2.405 pps
3.882 pps
4.203 NM
Practical Range
The practical range for the radar is less than the maximum theoretical range because the trace on the CRT (cathode ray tube) needs a period of time to return to the point of origin. This period is called the fly-back or dead time. During this period returning echoes cannot be displayed thereby reducing the range achievable for a given PRF.
11
Radar Principles 11
187
11 Radar Principles
Primary Radars
The pulses are concentrated into the beam dimensions designed for the particular radar. The beam uses the ‘echo’ principle to determine range and the ‘searchlight’ principle to indicate bearing or height. Figure 11.4 shows the Plan Position Indicator (PPI) display and Figure 11.5 shows the ATC radar antennae. The long structures at the top of the primary radar antennae are the secondary radar antennae.
The transmitter and receiver share the same antenna. The receiver is energized to accept ‘echoes’ from objects in the pulses’ path as soon as the transmitter pulse exits the antenna. The reflected pulses are very weak due to the double journey.
The shape and size of the radar antennae determines the size of the main and side lobes as well as the width of the radar beam generated by the system. The larger the aerial, the narrower will be the beam.
Principles Radar 11
Figure 11.4 A PPI display of primary raw radar
Figure 11.5 Typical radar antennae
188