- •Foreword
- •Preface
- •Contents
- •Symbols
- •1 Electromagnetic Field and Wave
- •1.1 The Physical Meaning of Maxwell’s Equations
- •1.1.1 Basic Source Variables
- •1.1.2 Basic Field Variables
- •1.1.3 Maxwell’s Equations in Free Space
- •1.1.4 Physical Meaning of Maxwell’s Equations
- •1.1.5 The Overall Physical Meaning of Maxwell’s Equations
- •1.2 Electromagnetic Power Flux
- •1.2.1 The Transmission of Electromagnetic Power Flux
- •1.2.2 Capacitors—Electrical Energy Storage
- •1.2.3 Inductor—Magnetic Energy Storage
- •1.2.4 Examples of Device Properties Analysis
- •1.3.1 Boundary Conditions of the Electromagnetic Field on the Ideal Conductor Surface
- •1.3.2 Air Electric Wall
- •2 Microwave Technology
- •2.1 The Theory of Microwave Transmission Line
- •2.1.1 Overview of Microwave Transmission Line
- •2.1.2 Transmission State and Cutoff State in the Microwave Transmission Line
- •2.1.3 The Concept of TEM Mode, TE Mode, and TM Mode in Microwave Transmission Line
- •2.1.4 Main Characteristics of the Coaxial Line [4]
- •2.1.5 Main Characteristics of the Waveguide Transmission Line
- •2.1.6 The Distributed Parameter Effect of Microwave Transmission Line
- •2.2 Application of Transmission Line Theories in EMC Research
- •3 Antenna Theory and Engineering
- •3.1 Field of Alternating Electric Dipole
- •3.1.1 Near Field
- •3.1.2 Far Field
- •3.2 Basic Antenna Concepts
- •3.2.1 Directivity Function and Pattern
- •3.2.2 Radiation Power
- •3.2.3 Radiation Resistance
- •3.2.4 Antenna Beamwidth and Gain
- •3.2.6 Antenna Feed System
- •4.1.1 Electromagnetic Interference
- •4.1.2 Electromagnetic Compatibility
- •4.1.3 Electromagnetic Vulnerability
- •4.1.4 Electromagnetic Environment
- •4.1.5 Electromagnetic Environment Effect
- •4.1.6 Electromagnetic Environment Adaptability
- •4.1.7 Spectrum Management
- •4.1.9 Spectrum Supportability
- •4.2 Essences of Quantitative EMC Design
- •4.2.2 Three Stages of EMC Technology Development
- •4.2.3 System-Level EMC
- •4.2.4 Characteristics of System-Level EMC
- •4.2.5 Interpretations of the EMI in Different Fields
- •4.3 Basic Concept of EMC Quantitative Design
- •4.3.1 Interference Correlation Relationship
- •4.3.2 Interference Correlation Matrix
- •4.3.3 System-Level EMC Requirements and Indicators
- •4.3.5 Equipment Isolation
- •4.3.6 Quantitative Allocation of Indicators
- •4.3.7 The Construction of EMC Behavioral Model
- •4.3.8 The Behavior Simulation of EMC
- •4.3.9 Quantitative Modeling Based on EMC Gray System Theory
- •5.2 Solution Method for EMC Condition
- •5.3 EMC Modeling Methodology
- •5.3.1 Methodology of System-Level Modeling
- •5.3.2 Methodology for Behavioral Modeling
- •5.3.3 EMC Modeling Method Based on Gray System Theory
- •5.4 EMC Simulation Method
- •6.1 EMC Geometric Modeling Method for Aircraft Platform
- •6.2.1 Interference Pair Determination and Interference Calculation
- •6.2.2 Field–Circuit Collaborative Evaluation Technique
- •6.2.3 The Method of EMC Coordination Evaluation
- •6.3 Method for System-Level EMC Quantitative Design
- •6.3.2 The Optimization Method of Single EMC Indicator
- •6.3.3 The Collaborative Optimization Method for Multiple EMC Indicators
- •7.1 The Basis for EMC Evaluation
- •7.2 The Scope of EMC Evaluation
- •7.2.1 EMC Design
- •7.2.2 EMC Management
- •7.2.3 EMC Test
- •7.3 Evaluation Method
- •7.3.1 The Hierarchical Evaluation Method
- •7.3.2 Evaluation Method by Phase
- •8 EMC Engineering Case Analysis
- •8.1 Hazard of Failure in CE102, RE102, and RS103 Test Items
- •8.2 The Main Reasons for CE102, RE102, and RS103 Test Failures
- •8.2.1 CE102 Test
- •8.2.2 RE102 Test
- •8.2.3 RS103 Test
- •8.3 The Solutions to Pass CE102, RE102, and RS103 Tests
- •8.3.1 The EMC Failure Location
- •8.3.2 Trouble Shooting Suggestions
- •A.1 Pre-processing Function
- •A.2 Post-processing Function
- •A.3 Program Management
- •A.4 EMC Evaluation
- •A.5 System-Level EMC Design
- •A.6 Database Management
- •References
Chapter 3
Antenna Theory and Engineering
This chapter explains the field generated by the alternating electric dipole, which is closely related to EMC research in the antenna theory and engineering [1, 7, 8]. Through this chapter, our readers will learn the basic characteristics of the near field, far field, and transition zone and understand that the EMC problems usually happens with the coexistence in the near field, far field, and transition zone. This chapter also explains the radiation characteristics of the antenna. Our readers will get the knowledge of some basic concepts of the antenna, including the antenna pattern and gain. In the last section, an example is provided to illustrate that the out-of-band characteristics of the antenna have become an important factor in the EMC design and antenna layout analysis of the whole aircraft.
3.1 Field of Alternating Electric Dipole
The field generated by the alternating electric dipole is closely related to EMC problems due to the leakage of fields from slots, apertures, and cables.
An alternating electric dipole refers to two alternating point charges +q(t) and −q(t), with the same value but opposite signs. The distance between the two point charges is dl(dl → 0), generally represented by qdl˙ . From the view of the law of charge conservation, alternating electric dipole qdl˙ can also be regarded as current element I˙dl
Let the time change factor be e− jωt , and then the electromagnetic field generated by the alternating dipole is [1]:
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H (r )
i ϕ |
˙ 4π |
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E(r) i rS ErS + i θ Eθ (r )
(3.1a)
(3.1b)
© National Defense Industry Press and Springer Nature Singapore Pte Ltd. 2019 |
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D. Su et al., Theory and Methods of Quantification Design on System-Level Electromagnetic Compatibility, https://doi.org/10.1007/978-981-13-3690-4_3
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3 Antenna Theory and Engineering |
where
˙ r ( )
E S r
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Eθ (r )
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I˙dl cos θ |
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2π ωε |
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rS2 − rS3 e− |
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4π ωε |
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I˙dl sin |
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For the sake of convenience, formulas (3.1a) and (3.1c) can be rewritten as
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H˙ ϕ (r ) |
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I˙dlβ |
2η2 cos θ |
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E˙ rS |
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where η μ ε is the wave impedance of the medium.
(3.2a)
(3.2b)
(3.2c)
The electromagnetic field excited by the alternating current elements represented by (3.1a)–(3.1c) is very important in the discussion of radiation problems. Next, we will analyze these three equations, which will lead to some basic concepts of radiation problems.
3.1.1 Near Field
The region that satisfies βrS << 1 is called the near-field region of the electric dipole. In the near-field region, there is
(βrS )−3 >> (βrS )−2 >> (βrS )−1
e−jβrS ≈ 1
Therefore, the magnetic field in the near-field region can be expressed as
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4π rS2 |
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i ϕ I dl |
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The electric field in the near-field region can be expressed as:
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2 cos θ + i θ sin θ |
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3.1 Field of Alternating Electric Dipole |
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It should be noted that the near-field magnetic field is exactly the same as the static magnetic field and the near-field electric field is identical with respect to the field excited by static electric dipole. Therefore, the near-field region is called as “quasistatic field.” From the Poynting vector of electromagnetic field, it can be concluded that the complex Poynting vector of the static field is a pure imaginary number with zero active power density. Therefore, the electromagnetic energy of the static field is not radiated, as if this part of the energy was trapped in the near zone. Therefore, the static field is usually called the “bounded field.” Based on this fact, we can say that the main component of the near-field region generated by the alternating electric dipole is the bounded field.
3.1.2 Far Field
The region which satisfies βrS >> 1 is the far-field region of the electric dipole. In the far field, since βrS >> 1, there is
(βrS )−1 >> (βrS )−2 >> (βrS )−3
Therefore, the magnetic field in the far-field region can be expressed as:
H˜ (r ) ≈ i φ jI˙dl |
sin θ e−jβrS |
A m |
2λrS |
The electric field in the far-field region can be expressed as:
E˜ (r ) ≈ i θ jη I˙dl |
sin θ e−jβrS |
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S˜ (r ) E˜ (r ) × H˜ (r ) 2 i rS η ˙φ |
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It indicates that there is an active power flow in the i rS direction, and the electromagnetic energy is propagating outward. In addition, from the expression of the electromagnetic field in the far field, the main part of the far field is inversely proportional to rS . Thus, their Poynting vector should be inversely proportional to rS2. Then, we can make a flux integral on the Poynting vector on the surface A of a sphere with the radius rS , and we will get a constant unrelated with rS , i.e.,
A S˜ (r ) · da |
π η I 2dl2 |
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