I. FUNDAMENTAL RADIATION THEORY & ANTENNA PARAMETERS
Retarded Potentials & Radiation from Elementary Sources
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Concept: The retarded potential accounts for the finite propagation speed ($c$) of EM waves. The potential at a point $\mathbf{r}$ and time $t$ depends on the source distribution at an earlier retarded time $$\displaystyle t_r = t - \frac{|\mathbf{r} - \mathbf{r}'|}{c} $$.
[!TIP] Core idea: Effects are not instantaneous. This is the foundation for all radiation calculations.
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Liénard-Wiechert Potentials: General solution for potentials from a moving point charge.
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Oscillating Electric Dipole (Hertzian Dipole): An infinitesimal current element $I\,dl$ with sinusoidal current $$\displaystyle I = I_0 e^{j\omega t} $$.
- Far-field ($r \gg \lambda$) Radiated Fields:
$$ \mathbf{E} \approx \frac{j\eta I_0 dl e^{-jkr}}{4\pi r} \sin\theta \, \hat{\theta} $$
$$ \mathbf{H} \approx \frac{j I_0 dl e^{-jkr}}{4\pi r} \sin\theta \, \hat{\phi} $$
where $$\displaystyle \eta = \sqrt{\mu_0/\varepsilon_0} $$, $$\displaystyle k = 2\pi/\lambda $$.
* **Time-Averaged Radiated Power**:
$$ P_{\text{rad}} = \frac{\eta I_0^2 (dl)^2}{12\pi^2} \left( \frac{2\pi}{\lambda} \right)^2 = \frac{\pi}{3} \eta I_0^2 \left( \frac{dl}{\lambda} \right)^2 \boxed{P_{\text{rad}} \propto (I_0 dl)^2 \cdot f^2} $$
Power $\propto$ square of frequency and square of dipole moment.
Antenna Characterization & Parameters
| Parameter | Definition | Key Point |
|---|---|---|
| Radiation Pattern | 3D plot of field/power vs. direction. | E-plane: contains $\mathbf{E}$ & propagation vector. H-plane: contains $\mathbf{H}$ & propagation vector. |
| Directivity ($D$) | Ratio of max radiation intensity to avg intensity. | $$\displaystyle D = \frac{4\pi}{A_e} $$ where $$\displaystyle A_e $$ is effective aperture. |
| Gain ($G$) | Directivity × Radiation Efficiency ($$\displaystyle \eta_r $$). | $$\displaystyle G = \eta_r D $$. Measured in dBi (w.r.t. isotropic) or dBd (w.r.t. dipole). |
| Beamwidth | Angular width between half-power points (HPBW). | Inversely related to directivity: $$\displaystyle D \approx \frac{4\pi}{\text{(HPBW)}^2} $$ for major lobe. |
| Radiation Resistance ($$\displaystyle R_r $$) | Equivalent resistance dissipating $$\displaystyle P_{\text{rad}} $$ as heat. | $$\displaystyle P_{\text{rad}} = \frac{1}{2} I_0^2 R_r $$ (for sinusoidal current). |
| Loss Resistance ($$\displaystyle R_l $$) | Resistance due to conductor/dielectric losses. | |
| Efficiency ($\eta$) | $$\displaystyle \eta = \frac{R_r}{R_r + R_l} $$. | |
| Effective Aperture ($$\displaystyle A_e $$) | Area capturing power from plane wave. | $$\displaystyle A_e = \frac{G \lambda^2}{4\pi} $$. |
| Effective Length ($$\displaystyle h_e $$) | Ratio of open-circuit voltage to incident $\mathbf{E}$-field. | $$\displaystyle V_{oc} = h_e E_{\text{inc}} $$ for linear polarization. |
| Reciprocity Theorem | TX and RX patterns are identical for same antenna. | $$\displaystyle h_e $$ (RX) = $$\displaystyle h_e $$ (TX). Fundamental for antenna measurements. |
Near-field and Far-field Regions
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Reactive Near-field (Fresnel): $$\displaystyle r < 0.62\sqrt{D^3/\lambda} $$ (D = largest antenna dim.). Field energy stored, not radiating. $\mathbf{E}$ & $\mathbf{H}$ out of phase, complex impedance.
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Radiating Far-field (Fraunhofer): $$\displaystyle r > \frac{2D^2}{\lambda} $$. Fields are:
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Transverse ($$\displaystyle E_\theta, H_\phi $$ only).
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$$\displaystyle |\mathbf{E}|/|\mathbf{H}| = \eta $$ (intrinsic impedance of medium).
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Angularly independent of $r$.
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$\mathbf{E}$ & $\mathbf{H}$ in phase.
[!TIP] Far-field approximation assumes $r \gg \lambda$ and $r \gg D$, allowing $|\mathbf{r}-\mathbf{r}'| \approx r - \hat{r}\cdot\mathbf{r}'$ in phase term and $1/|\mathbf{r}-\mathbf{r}'| \approx 1/r$ in amplitude.
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Antenna Analysis Principles
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Pattern Multiplication Theorem: Radiation pattern of an array = Array Factor (AF) × Element Pattern.
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AF depends on geometry, amplitude, phase of array.
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Element pattern is pattern of a single antenna.
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Babinet's Principle: For complementary apertures (e.g., slot & dipole) in infinite conducting plane:
$$ \mathbf{E}_{\text{slot}} = \eta_0 \hat{n} \times \mathbf{H}_{\text{dipole}}, \quad \mathbf{H}_{\text{slot}} = -\frac{\hat{n} \times \mathbf{E}_{\text{dipole}}}{\eta_0} $$
* **Impedance relation**: $$\displaystyle Z_{\text{slot}} Z_{\text{dipole}} = \eta_0^2/4 $$.
- Equivalence Principle: Replaces actual sources with equivalent electric/magnetic surface currents on a closed surface to compute fields outside.
II. WIRE ANTENNAS & BASIC ELEMENTS
Short Dipole & Monopole
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Short Dipole ($L \ll \lambda$): Current ~ constant ($$\displaystyle I_0 $$). Radiation pattern: Figure-8 in E-plane ($\sin\theta$), omnidirectional in H-plane.
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Quarter-wave Monopole over perfect ground plane:
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Image Theory: Replace ground with image of monopole (inverted). Creates half-wave dipole in free space.
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Radiation Pattern: Same as half-wave dipole in upper hemisphere only. Gain = $2 \times$ gain of half-wave dipole (since power radiated only into $2\pi$ steradians) → $G \approx 5.15$ dBi (or 3.15 dBd).
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Input Impedance: $$\displaystyle Z_{\text{in}} \approx 36.5 + j21.25\ \Omega $$ (resistance ≈ half of half-wave dipole's 73Ω).
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Applications: Mobile/vehicle antennas, mast radiators.
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Half-wave Dipole
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Current distribution: $$\displaystyle I(z) = I_0 \cos(kz) $$.
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Input Impedance: $$\displaystyle Z_{\text{in}} \approx 73 + j42.5\ \Omega $$. Standard reference antenna.
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Radiation Resistance: $$\displaystyle R_r \approx 73\ \Omega $$.
Long Wire & Travelling Wave Antennas
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Long Wire Antenna ($$\displaystyle L > \lambda $$):
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Current: Travelling wave (not standing wave). $$\displaystyle I(z) = I_0 e^{-j\beta z} $$.
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Radiation: Main lobe at angle $$\displaystyle \theta_m $$ where $$\displaystyle \sin\theta_m = \frac{\lambda}{L} $$ (for $L \gg \lambda$). End-fire direction.
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Pattern: Multiple lobes (grating lobes). Number of lobes ≈ $L/\lambda$.
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Length Influence: Longer wire → narrower main lobe, more lobes.
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V Antenna: Two long wires at angle. Main lobe along bisector.
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Rhombic Antenna: Four-wire diamond shape. Travelling wave terminated with resistor. Wideband, high gain (10-15 dBi), unidirectional. Used for HF point-to-point.
Folded Dipole & Variants
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Folded Dipole: Two parallel $\lambda/2$ dipoles connected at ends. Fed at center of one.
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Input Impedance: $\approx 4 \times$ impedance of single dipole → $\approx 300\ \Omega$. Wider bandwidth than simple dipole.
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Current: Equal magnitude, opposite phase in two arms.
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Turnstile Antenna (Crossed Dipoles):
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Two $\lambda/2$ dipoles crossed at center, fed with $$\displaystyle 90^\circ $$ phase shift.
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Axial Mode: Circularly polarized radiation along axis (broadside). Applications: Satellite comms, FM broadcasting (for CP reception).
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Log-Periodic Antenna:
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Structure: Series of driven elements with lengths & spacing increasing by factor $\tau$ (scale factor). Feed via transmission line crossing all elements.
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Frequency-Independent Principle: Input impedance & radiation pattern repeat periodically with $\log(f)$. Wideband (octave+).
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Active Region: Only 1-3 elements radiate effectively at a given frequency.
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III. ANTENNA ARRAYS
Array Fundamentals & Analysis
- Array Factor (AF) for N isotropic sources with spacing $d$, progressive phase $\beta$:
$$ \text{AF} = \sum_{n=0}^{N-1} I_n e^{j n (\psi + \beta)}, \quad \psi = kd \cos\theta $$
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Broadside Array: $$\displaystyle \beta = 0 $$, main lobe at $$\displaystyle \theta = 90^\circ $$.
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End-fire Array: $$\displaystyle \beta = \pm kd $$, main lobe at $$\displaystyle \theta = 0^\circ $$ or $$\displaystyle 180^\circ $$. Hansen-Woodyard condition for optimum: $$\displaystyle \beta = \pm (kd + \delta) $$ with $\delta \approx 0.226(kd)$.
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Scanning: To steer beam to $$\displaystyle \theta_0 $$, set $$\displaystyle \beta = -kd \cos\theta_0 $$.
Array Synthesis Methods
| Method | Sidelobe Level | Beamwidth | Trade-off |
|---|---|---|---|
| Uniform | $-13.2$ dB (first sidelobe) | Narrowest | High sidelobes |
| Binomial | No sidelobes (theoretical) | Widest | Poor taper, wide main lobe |
| Dolph-Chebyshev | Preset (e.g., $-30$ dB) | Slightly wider than uniform | Optimal for given SLL |
| Taylor (Sum pattern) | Preset first few SLLs, others decay as $$\displaystyle 1/(n^2 + \gamma^2) $$ | Near-optimal | Practical for large arrays |
- Schelkunoff Unit Circle Method: Graphical synthesis. Plot array coefficients on unit circle. Zeros of AF correspond to roots on circle. Enables design for null placement.
Practical Wire Arrays
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Yagi-Uda Antenna:
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Elements: 1 driven (dipole), 1 reflector (longer, behind), multiple directors (shorter, in front).
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Mechanism: Reflector induces current with phase lag → forward reinforcement. Directors induce current with phase lead → forward reinforcement.
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Pattern: Unidirectional, high gain (7-15 dBi), narrow bandwidth (≈5%).
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Applications: TV reception, point-to-point links.
[!TIP] Key: Reflector length $\approx 0.5\lambda$, spacing $\approx 0.15-0.2\lambda$. Director lengths $\approx 0.45-0.48\lambda$, spacing decreasing.
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Log-Periodic: Already covered.
Planar & Aperture Distributions
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Uniform Aperture: $$\displaystyle J(\mathbf{r}') = \text{constant} $$. Narrowest beamwidth but high first sidelobe ($-13.2$ dB).
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Tapered Aperture (e.g., Taylor, Chebyshev): Amplitude tapers to edges.
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Advantage: Reduced sidelobes.
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Disadvantage: Wider main lobe and reduced aperture efficiency.
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Horizontal Patterns in Broadcast Arrays:
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AM broadcast towers use phased arrays to shape horizontal pattern.
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Goal: Concentrate radiation in service area, minimize radiation in undesired directions (e.g., to avoid interference).
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Control: By adjusting amplitudes & phases of multiple towers.
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IV. APERTURE & REFLECTOR ANTENNAS
Horn Antennas
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Types: Pyramidal (rectangular), Conical, Sectoral (E-plane/H-plane), Corrugated (low cross-pol, wideband).
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Radiation Mechanism: Aperture field is TE$$\displaystyle _{10} $$ mode from waveguide. Phase error across aperture limits gain.
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Aperture Efficiency ($$\displaystyle \eta_a $$): $$\displaystyle \eta_a = \eta_r \eta_p \eta_s $$ (spillover, phase, blockage efficiencies). Typical $$\displaystyle \eta_a \approx 0.5-0.6 $$.
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Gain: $$\displaystyle G = \frac{4\pi A_e}{\lambda^2} = \eta_a \frac{4\pi A_{\text{phys}}}{\lambda^2} $$.
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Gain Measurement (Gain Comparison): Compare received power with standard gain horn at same distance.
Parabolic Reflector Antennas
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Principle: Parallel rays from feed reflect off parabola → converge at focus (or vice versa). Phase error zero on-axis.
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Feed Mechanisms:
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Axial (Prime Focus): Feed at focus. Simple, large aperture blockage by feed & supports.
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Cassegrain: Subreflector (hyperbolic) reflects to feed at vertex. Lower blockage, higher gain.
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Gregorian: Ellipsoidal subreflector. Larger focal length, less sensitive to feed illumination.
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Aperture Blockage: Caused by feed, subreflector, supports.
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Effects: Reduces gain, increases sidelobes, distorts pattern.
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Mitigation: Use transparent subreflectors, offset feeds (Offset Parabola).
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Surface Accuracy: RMS surface error $\sigma$ causes gain reduction: $$\displaystyle \eta_s \approx e^{-(4\pi\sigma/\lambda)^2} $$ (Ruze's formula).
Slot & Complementary Antennas
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Slot Antenna: Slot in conducting plane. Radiates when fed (e.g., waveguide).
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Babinet's Principle Applied:
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Slot in infinite ground plane $$\displaystyle \leftrightarrow $$ Dipole of complementary shape in free space.
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Radiation Pattern: Slot pattern is identical to dipole pattern but with $\mathbf{E}$ & $\mathbf{H}$ interchanged, and $\theta$ & $\phi$ swapped.
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Rectangular Slot ($a \times b$):
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$$\displaystyle E_\phi $$ (co-pol) $$\displaystyle \propto \frac{\sin(kb\sin\theta\cos\phi/2)}{(kb\sin\theta\cos\phi/2)} \cdot \frac{\sin(ka\sin\theta\sin\phi/2)}{(ka\sin\theta\sin\phi/2)} $$
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Pattern similar to thin dipole ($b \ll \lambda$, $a \approx \lambda/2$).
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Microstrip (Patch) Antenna:
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Construction: Metallic patch on dielectric substrate over ground plane.
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Radiation Mechanism: Fringing fields at edges. Cavity model: Patch acts as resonant cavity.
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Feeding: Microstrip line, probe, aperture coupling.
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Advantages: Low profile, conformal, lightweight, inexpensive, easy to integrate.
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Limitations: Narrow bandwidth (1-5%), low efficiency (due to substrate losses), low power handling.
[!TIP] RGPV focus: Design equations (Transmission Line Model):
- Width: $$\displaystyle W = \frac{c}{2f_r\sqrt{\frac{\varepsilon_r+1}{2}}} $$
- Effective dielectric: $$\displaystyle \varepsilon_{\text{eff}} = \frac{\varepsilon_r+1}{2} + \frac{\varepsilon_r-1}{2}(1+12h/W)^{-1/2} $$
- Length: $$\displaystyle L = \frac{c}{2f_r\sqrt{\varepsilon_{\text{eff}}}} - 2\Delta L $$, $$\displaystyle \Delta L \approx 0.412h\frac{(\varepsilon_{\text{eff}}+0.3)(W/h+0.264)}{(\varepsilon_{\text{eff}}-0.258)(W/h+0.8)} $$
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V. SPECIALIZED & PRINTED ANTENNAS
Microstrip Antennas (Patch) - Details
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Substrate Parameters: Higher $$\displaystyle \varepsilon_r $$ → smaller size, narrower bandwidth, more surface waves. Lower $h$ → narrower bandwidth, higher field concentration.
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Polarization: Linear (along width). Circular via sequential rotation or perturbed square patch.
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Arrays: Series/parallel feeds, corporate feeds for high gain.
Helical Antenna
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Normal Mode ($L \approx N\lambda/10$, $D \approx \lambda/10$):
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Current ~ uniform, radiation similar to short dipole.
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Broadside pattern (perpendicular to helix axis).
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Applications: Low-gain, compact antennas for handheld devices.
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Axial Mode ($L \approx N\lambda$, $D \approx 0.1-0.3\lambda$, $C \approx \lambda$):
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Current Travelling wave along helix.
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Radiation: Maximum along helix axis (end-fire).
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Circular Polarization (sense determined by winding direction).
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Gain: $$\displaystyle G \approx 15 \left( \frac{C}{\lambda} \right)^{2.5} \left( \frac{N\lambda}{L} \right) $$ (Balmain's formula).
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Bandwidth: Wide (octave+). Applications: Satellite comms, deep-space.
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Lens Antennas
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Types:
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Dielectric Lens: Slow wave medium, focuses like optical lens.
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Zoned Lens: Reduces thickness & weight by removing annular sections.
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Artificial Lens (Metamaterial): Uses subwavelength structures.
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Principle: Corrects phase of spherical wave from feed to planar wavefront.
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Advantages: High gain, low spillover loss.
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Disadvantages: Heavy (dielectric), expensive, narrowband (dielectric constant variation).
VI. GROUND EFFECTS & ENVIRONMENTAL IMPACT
Effect of Ground on Antenna Patterns
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Image Theory:
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Perfect Electric Conductor (PEC): Image current same magnitude, opposite direction for vertical dipole; same direction for horizontal dipole.
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Imperfect Ground: Complex reflection coefficient $$\displaystyle \Gamma = |\Gamma|e^{j\psi} $$ depends on angle of incidence, conductivity $\sigma$, permittivity $$\displaystyle \varepsilon_r $$.
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Impact on Vertical Patterns:
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Vertical Dipole (over ground): Pattern is combination of direct + ground-reflected waves.
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Low-angle radiation (critical for ground wave, sky wave) is strongly affected by ground conductivity.
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Good ground ($\sigma$ high, e.g., sea water): High reflection, constructive interference at low angles → elevated low-angle lobes.
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Poor ground ($\sigma$ low, e.g., dry sand): Low reflection, destructive interference → depressed low-angle lobes.
[!TIP] For vertical polarization, ground reflection coefficient $$\displaystyle \Gamma_\parallel $$ is negative for grazing incidence → phase reversal → pattern null at horizon for perfect ground.
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Horizontal Dipole: Image same phase → pattern reinforced at low angles.
General Environmental Effects
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Atmosphere: Refractive index decreases with height → bending (refraction) of rays downward (standard refraction).
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Terrain: Hills/buildings cause diffraction, scattering, shadowing.
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Obstacles: Attenuate signals, cause multipath.
VII. RADIO WAVE PROPAGATION MECHANISMS
Ground Wave Propagation
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Components:
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Direct Wave: Line-of-sight.
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Ground-Reflected Wave: From earth's surface.
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Surface Wave: Bound to earth's surface, follows curvature. Dominant for LF/MF.
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Transition Surface ↔ Space Wave: At some distance, surface wave becomes negligible compared to space wave (direct + reflected). This transition distance depends on frequency, antenna height, ground properties.
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Effect of Terrain: Smooth, conductive ground (sea) → longer transition, better propagation. Rough, poor ground → shorter transition, higher attenuation.
Sky Wave (Ionospheric) Propagation
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Ionosphere Layers: D (60-90 km, daytime only, absorbs LF), E (90-120 km), F (150-400 km, splits into F1/F2 day).
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Critical Frequency ($$\displaystyle f_c $$): Max frequency that will be reflected back vertically.
$$ f_c = 9\sqrt{N_{\text{max}}} \ \text{Hz}, \quad N_{\text{max}} = \text{peak electron density (m}^{-3}\text{)} $$
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Virtual Height ($h'$): Apparent height from which wave appears reflected (due to bending).
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MUF (Maximum Usable Frequency): Max frequency that can be used for a given path via a specific layer at angle $$\displaystyle \theta_i $$.
$$ \boxed{\text{MUF} = f_c \sec\theta_i} $$
where $$\displaystyle \theta_i $$ is angle of incidence at ionosphere.
- Skip Distance ($$\displaystyle d_s $$): Minimum distance from transmitter where sky wave returns to earth.
$$ d_s = 2h' \tan\theta_i $$
- Relation between MUF and Skip Distance:
$$ \boxed{d_s = 2h' \sqrt{\left(\frac{\text{MUF}}{f_c}\right)^2 - 1}} $$
> [!TIP] Derivation: From MUF = $$\displaystyle f_c \sec\theta_i $$, so $$\displaystyle \tan\theta_i = \sqrt{\sec^2\theta_i - 1} = \sqrt{(\text{MUF}/f_c)^2 - 1} $$. Then $$\displaystyle d_s = 2h' \tan\theta_i $$.
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LUF (Lowest Usable Frequency): Min frequency that can be received with acceptable signal-to-noise ratio. Limited by atmospheric noise at lower frequencies.
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Day/Night: D-layer disappears at night → lower absorption → better HF propagation. F-layer higher at night → lower MUF.
Space Wave & Tropospheric Propagation
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Direct + Ground-Reflected: Resultant pattern depends on antenna heights, phase difference.
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Super Refraction: Refractive index decreases rapidly with height ($$\displaystyle dN/dh < -157 $$ N-units/km). Rays bend more than normal → extends radio horizon.
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Sub Refraction: $$\displaystyle dN/dh > -157 $$ N-units/km. Rays bend less → reduces radio horizon.
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Tropospheric Scattering: Turbulence in troposphere causes forward scattering of UHF/SHF signals beyond horizon. Scatter volume at common volume of TX/RX beams. Applications: Beyond-line-of-sight comms (100-500 km).
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Tropospheric Ducts:
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Surface Duct: Strong inversion near ground (e.g., over cool water). Traps waves, propagates with low loss over hundreds of km.
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Elevated Duct: Inversion at 100s of meters. Common over oceans.
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Evaporation Duct: Over water, humidity gradient forms duct ~10-40 m high.
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Radius of Curvature of Ray Path:
In a stratified atmosphere with refractive index $n(h)$ decreasing linearly: $$\displaystyle n(h) = n_0 - \alpha h $$.
$$ \boxed{R = \frac{1}{\alpha} = \frac{n_0}{\left| \frac{dn}{dh} \right|}} $$
For standard atmosphere, $$\displaystyle R \approx 4/3 \times R_{\text{earth}} $$ (effective Earth radius factor $$\displaystyle k = 4/3 $$).
VIII. NUMERICAL TOOLS & ADVANCED TOPICS
Numerical Methods for Antenna Analysis
| Method | Principle | Best For |
|---|---|---|
| MoM (Method of Moments) | Integral equation, basis functions. | Wire antennas, surfaces. |
| FEM (Finite Element Method) | Variational, domain discretization. | Complex dielectrics, cavities. |
| FDTD (Finite-Difference Time-Domain) | Time-stepping on Yee grid. | Broadband, transient, complex media. |
| FIT (Finite Integration Technique) | Discrete form of Maxwell's equations. | General purpose (CST Studio). |
Other Specialized Topics (Brief)
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Flat Sheet & Corner Reflectors: Flat sheet (planar reflector) increases gain of dipole by ~2-3 dB. Corner reflector (two flat sheets at $$\displaystyle 90^\circ $$) gives higher gain (~8-10 dB) and unidirectional pattern.
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Feeding Structures: Probe (conducting pin), aperture (slot), microstrip line, etc. Choice affects bandwidth, cross-pol.
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V Antenna: Already covered in long wire.
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Parabolic Reflector Design: Key considerations: f/D ratio (focal length/diameter) affects spillover, blockage, phase error. Typical $f/D \approx 0.3-0.5$. Surface tolerance $$\displaystyle \sigma < \lambda/50 $$ for high efficiency.