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11.3 Antenna Principles & Electromagnetic Wave Propagation

Key Takeaways

  • An ideal isotropic radiator emits electromagnetic energy uniformly in all directions with a baseline gain of 0 dBi (equivalent to -2.15 dBd relative to a half-wave dipole).

  • The physical resonant length of a half-wave dipole in free space is L = 143 / f_MHz meters (accounting for a 5% end-effect velocity factor).

  • The Friis Free-Space Transmission Equation calculates received signal power Pr = Pt * Gt * Gr * (lambda / (4 * pi * d))^2, demonstrating inverse-square distance loss.

  • Ionospheric Maximum Usable Frequency is defined by the Secant Law: MUF = fc / cos(theta) = fc * sec(theta), where fc is critical frequency.

  • EM wave propagation mechanisms encompass Surface/Ground Waves (<2 MHz), Ionospheric Skywaves (2-30 MHz), and Line-of-Sight Space Waves (>30 MHz).

Last updated: July 2026

11.3 Antenna Principles & Electromagnetic Wave Propagation

Quick Answer: Antennas couple guided electromagnetic energy to unguided space waves. Key PRC licensure formulas include resonant half-wave dipole length (L=143/fMHzL = 143 / f_{\text{MHz}} meters), antenna gain conversion (GdBi=GdBd+2.15G_{\text{dBi}} = G_{\text{dBd}} + 2.15), radio horizon distance (dkm=3.57[ht+hr]d_{\text{km}} = 3.57 [\sqrt{h_t} + \sqrt{h_r}]), ionospheric Maximum Usable Frequency (MUF=fc⋅sec⁡θMUF = f_c \cdot \sec \theta), and Free-Space Path Loss (FSPLdB=32.44+20log⁡10fMHz+20log⁡10dkmFSPL_{\text{dB}} = 32.44 + 20 \log_{10} f_{\text{MHz}} + 20 \log_{10} d_{\text{km}}).


Antenna Fundamentals & Radiation Mechanism

An antenna (or aerial) is a metallic conductor or structure that acts as a transducer between a guided electrical wave traveling along a transmission line and an unguided electromagnetic (EM) wave propagating in free space. Radiation occurs when alternating electric currents accelerate along a conductor, detaching electric (E⃗\vec{E}) and magnetic (H⃗\vec{H}) fields that propagate orthogonally to each other and to the direction of propagation.


Key Antenna Performance Parameters

  1. Isotropic Radiator: A theoretical point-source antenna that radiates energy equally in all directions, producing a spherical wavefront. Serves as the fundamental reference (0 dBi0 \text{ dBi}).
  2. Half-Wave Dipole ( λ/2\,\lambda / 2 Dipole): The standard physical reference antenna. Radiates a doughnut-shaped omnidirectional pattern in its azimuth plane, possessing a directivity gain of 2.15 dBi2.15 \text{ dBi} (1.641.64 linear gain) and a radiation resistance of 73 Ω73 \ \Omega at resonance. GdBi=GdBd+2.15G_{\text{dBi}} = G_{\text{dBd}} + 2.15
  3. Directive Gain (GG) & Directivity (DD): Directivity is the ratio of radiation intensity in a specific direction to the average radiation intensity in all directions. Gain incorporates antenna efficiency η\eta (0≤η≤10 \le \eta \le 1): G=η⋅DG = \eta \cdot D
  4. Half-Power Beamwidth (HPBW): The angular width of the main lobe measured between the two points where radiated power density drops to half (−3 dB-3 \text{ dB}) of its maximum peak.
  5. Polarization: The spatial orientation of the electric field vector (E⃗\vec{E}) radiated by the antenna (Vertical, Horizontal, Circular, or Elliptical).

Practical Antenna Sizing Formulas

Due to the finite thickness of antenna conductors and capacitive end-effect, EM waves travel approximately 5%5\% slower along metallic conductors than in free space (velocity factor vf≈0.95v_f \approx 0.95).

                    ◄────────────── Length L ──────────────►
                     ┌──────────────────┐┌──────────────────┐
                     │  Dipole Arm 1    ││  Dipole Arm 2    │
                     └────────┬─────────┘└─────────┬────────┘
                              │   Feedline 73Ω    │
                              └─────────┐ ┌───────┘
                                        │ │

Resonant Half-Wave Dipole Antenna

For a center-fed half-wave dipole, the physical length LL is:

Lmeters=0.95⋅c2f=143fMHz(or Lfeet=468fMHz)L_{\text{meters}} = \frac{0.95 \cdot c}{2 f} = \frac{143}{f_{\text{MHz}}} \quad \left(\text{or } L_{\text{feet}} = \frac{468}{f_{\text{MHz}}}\right)

Quarter-Wave Vertical Monopole Antenna

A quarter-wave monopole mounted over a perfectly conducting ground plane utilizes image theory to form a virtual half-wave dipole, exhibiting a 36.5 Ω36.5 \ \Omega radiation resistance:

Lmonopole, meters=71.5fMHz(or Lfeet=234fMHz)L_{\text{monopole, meters}} = \frac{71.5}{f_{\text{MHz}}} \quad \left(\text{or } L_{\text{feet}} = \frac{234}{f_{\text{MHz}}}\right)

Common Antenna Configurations

  • Yagi-Uda Array: End-fire directional array comprising a driven element (half-wave dipole), a slightly longer reflector placed behind (+5%+5\% length), and one or more shorter directors (−5%-5\% length) placed in front.
  • Parabolic Reflector Dish: High-gain aperture antenna used for microwave and satellite links. Parabolic surface reflects rays into a parallel beam. Gain equation: G=η(πDλ)2G = \eta \left(\frac{\pi D}{\lambda}\right)^2 where DD is dish diameter, λ\lambda is wavelength, and η\eta is aperture efficiency (typically 55%−70%55\% - 70\%).

Electromagnetic Wave Propagation Modes

EM waves travel from transmitter to receiver via three primary modes:

  Ionosphere Layer (Skywave Refraction: 2 - 30 MHz)
 ─────────────────────────────────────────────────────────────
       ▲                                        │
       │ Skywave                                │ Refracted Skywave
       │                                        ▼
   ┌───┴───┐                                ┌───┴───┐
   │ TX    │=== Direct Line-of-Sight =====>│ RX    │ (Space Wave: > 30 MHz)
   └───┬───┘   (Space Wave: > 30 MHz)       └───┬───┘
  ─────┴────────────────────────────────────────┴─────────────
       Ground/Surface Wave Diffraction (< 2 MHz)
  1. Ground Wave (Surface Wave) Propagation (<2 MHz< 2 \text{ MHz}): Waves tilt and follow the curvature of the Earth due to ground diffraction and induced surface currents. Used for VLF/LF/MF broadcast radio (AM radio 535−1705 kHz535 - 1705 \text{ kHz}). Severely attenuated over land; travels best over saltwater.
  2. Skywave Propagation (2 MHz−30 MHz2 \text{ MHz} - 30 \text{ MHz}): High Frequency (HF) waves hit the ionized upper atmosphere (Ionosphere) and refract (bend) back to Earth, enabling transoceanic long-distance communications beyond the horizon.
  3. Space Wave (Direct & Ground-Reflected) Line-of-Sight (>30 MHz> 30 \text{ MHz}): VHF, UHF, and microwave signals penetrate the ionosphere into space without bending back. Propagation is restricted to direct Line-of-Sight (LOS).

Radio Horizon Calculation

Due to atmospheric refraction (4/34/3 effective Earth radius factor), the radio horizon extends slightly beyond the optical horizon:

dLOS, km=3.57(ht+hr)d_{\text{LOS, km}} = 3.57 \left(\sqrt{h_t} + \sqrt{h_r}\right)

where hth_t and hrh_r are transmitter and receiver antenna heights above ground in meters.


Ionospheric Skywave Propagation & Formulas

The ionosphere contains ionized atmospheric layers (D,E,F1,F2D, E, F_1, F_2) formed by solar ultraviolet radiation.

  • D Layer (60-90 km): Exists only during daytime; absorbs HF waves (<3 MHz< 3 \text{ MHz}).
  • E Layer (90-130 km): Refracts upper MF and lower HF waves during the day.
  • F Layer (150-400 km): Splices into F1F_1 and F2F_2 layers by day and merges into a single FF layer by night. Primary ionospheric layer for long-distance HF skip communications.

Critical Frequency (fcf_c)

The highest frequency that returns to Earth when transmitted straight up vertically (90∘90^\circ incidence):

fc=9Nmaxf_c = 9 \sqrt{N_{max}}

where NmaxN_{max} is maximum electron density in electrons/m3\text{electrons/m}^3.

Maximum Usable Frequency (MUF)

The highest frequency that can be used for skywave communication between two specific points at an angle of incidence θ\theta (Secant Law):

MUF=fccos⁡θ=fc⋅sec⁡θMUF = \frac{f_c}{\cos \theta} = f_c \cdot \sec \theta

Optimum Working Frequency (OWF / FOT)

To protect against ionospheric diurnal variations, the operational frequency is chosen as 85%85\% of MUF:

OWF=0.85×MUFOWF = 0.85 \times MUF

Free-Space Path Loss & Friis Link Equation

In an ideal unobstructed free space, power density decreases with the square of distance.

Friis Transmission Equation

Pr=Pt⋅Gt⋅Gr(λ4πd)2P_r = P_t \cdot G_t \cdot G_r \left(\frac{\lambda}{4 \pi d}\right)^2

where PrP_r is received power, PtP_t is transmit power, Gt,GrG_t, G_r are antenna linear gains, and dd is path distance.

Free-Space Path Loss (FSPL) Formula in Decibels

Converting the loss factor (4πd/λ)2(4\pi d / \lambda)^2 into logarithmic decibel form yields the mandatory board exam formula:

FSPLdB=32.44+20log⁡10(fMHz)+20log⁡10(dkm)FSPL_{\text{dB}} = 32.44 + 20 \log_{10}(f_{\text{MHz}}) + 20 \log_{10}(d_{\text{km}})

(Alternatively, if frequency is in GHz: FSPLdB=92.45+20log⁡10(fGHz)+20log⁡10(dkm)FSPL_{\text{dB}} = 92.45 + 20 \log_{10}(f_{\text{GHz}}) + 20 \log_{10}(d_{\text{km}})).


Step-by-Step Path Loss Calculation Example

Problem: A line-of-sight wireless telemetry link operates at 2.4 GHz2.4 \text{ GHz} (2400 MHz2400 \text{ MHz}) across a distance of 10 km10 \text{ km}. Calculate the Free-Space Path Loss (FSPLFSPL) in decibels.

Solution:

  1. Identify Given Values: f=2400 MHzf = 2400 \text{ MHz}, d=10 kmd = 10 \text{ km}.
  2. Apply FSPL Equation: FSPLdB=32.44+20log⁡10(2400)+20log⁡10(10)FSPL_{\text{dB}} = 32.44 + 20 \log_{10}(2400) + 20 \log_{10}(10)
  3. Calculate Logarithms: log⁡10(2400)≈3.3802→20×3.3802=67.60 dB\log_{10}(2400) \approx 3.3802 \rightarrow 20 \times 3.3802 = 67.60 \text{ dB} log⁡10(10)=1.0000→20×1.0000=20.00 dB\log_{10}(10) = 1.0000 \rightarrow 20 \times 1.0000 = 20.00 \text{ dB}
  4. Sum Components: FSPLdB=32.44+67.60+20.00=120.04 dBFSPL_{\text{dB}} = 32.44 + 67.60 + 20.00 = 120.04 \text{ dB}
Test Your Knowledge

What is the physical resonant length of a half-wave dipole antenna designed to operate at an FM broadcast frequency of 100 MHz in free space?

A

1.43 meters

B

2.86 meters

C

0.715 meters

D

4.68 meters

Test Your Knowledge

An HF ionospheric sounding station measures a vertical critical frequency (fc) of 8 MHz. If the angle of incidence for a distant skywave link is 60 degrees, what is the Maximum Usable Frequency (MUF)?

A

4.0 MHz

B

9.24 MHz

C

16.0 MHz

D

13.86 MHz

Test Your Knowledge

A transmitter tower has an antenna height of 49 meters above ground, and a receiving mobile tower has an antenna height of 16 meters. What is the maximum line-of-sight radio horizon distance between them?

A

24.99 km

B

39.27 km

C

17.85 km

D

54.60 km

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