ECE 4370: Antenna Engineering Solutions to TEST 1 (Fall 2017) · 2020. 7. 31. · ECE 4370: Antenna...

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ECE 4370: Antenna Engineering Solutions to TEST 1 (Fall 2017) 1. Antenna Recognition: 1. Half-Wave Dipole (b) 5. Meandered Dipole (a) 2. λ 4 -Monopole (c) 6. Biconical Antenna (d) 3. Patch Antenna (h) 7. Loop Antenna (f) 4. Folded Dipole (g) 8. Broadband Monopole (e) 2. Directivity: Directivity must average to 1 over 4π steradians. If an antenna radiates into an octant with directivity D 0 and radiates into the remaining 7 octants with directivity 0, then D 0 must equal 8 in the linear scale (9 dBi). 3. Shortened Dipole: (a) Neglecting the coupling between meandered horizontal segments, this resonating antenna should be λ/2 in length when straightened. (b) Start with the vector magnetic potential, making the same phase approximation for the electrically short dipole: ˜ A z (r, θ, φ)= μ 4πr exp (-jkr) + L 2 Z - L 2 I cos z 0 π L exp(+jkz 0 cosθ | {z } 0 ) dz 0 = μIL 2π 2 r exp (-jkr) From this we arrive at the far-field electric and magnetic field solutions: ˜ ~ H(r, φ, θ) jkIL sin θ 2π 2 r exp (-jkr) ˆ φ ˜ ~ E(r, φ, θ) jkηIL sin θ 2π 2 r exp (-jkr) ˆ θ 1

Transcript of ECE 4370: Antenna Engineering Solutions to TEST 1 (Fall 2017) · 2020. 7. 31. · ECE 4370: Antenna...

  • ECE 4370: Antenna Engineering

    Solutions to TEST 1 (Fall 2017)

    1. Antenna Recognition:

    (b) (c)(a)

    (e) (f) (g)

    (d)

    (h)

    1. Half-Wave Dipole (b) 5. Meandered Dipole (a)

    2. λ4 -Monopole (c) 6. Biconical Antenna (d)

    3. Patch Antenna (h) 7. Loop Antenna (f)

    4. Folded Dipole (g) 8. Broadband Monopole (e)

    2. Directivity: Directivity must average to 1 over 4π steradians. If an antenna radiates into anoctant with directivity D0 and radiates into the remaining 7 octants with directivity 0, thenD0 must equal 8 in the linear scale (9 dBi).

    3. Shortened Dipole:

    (a) Neglecting the coupling between meandered horizontal segments, this resonating antennashould be λ/2 in length when straightened.

    (b) Start with the vector magnetic potential, making the same phase approximation for theelectrically short dipole:

    Ãz(r, θ, φ) =µ

    4πrexp (−jkr)

    +L2∫−L2

    I cosz′π

    Lexp(+jkz′ cosθ︸ ︷︷ ︸

    ≈0

    ) dz′ =µIL

    2π2rexp (−jkr)

    From this we arrive at the far-field electric and magnetic field solutions:

    ~̃H(r, φ, θ) ≈ jkIL sin θ2π2r

    exp (−jkr) φ̂ ~̃E(r, φ, θ) ≈ jkηIL sin θ2π2r

    exp (−jkr) θ̂

    1

  • (c) 90 degrees (identical to the Hertzian and electrically short dipoles)

    (d) We neet to calculate total radiated power for this:

    PT =

    2π∫0

    π∫0

    ~Sav︷ ︸︸ ︷1

    2~̃E × ~̃H

    ∗·r2 sin θ dθ dφ r̂

    =

    2π∫0

    π∫0

    1

    2

    kηIL sin θ

    2π2r

    kIL sin θ

    2π2rr2 sin θ dθ dφ

    = 2πηk2I2L2

    8π4

    π∫0

    sin3 θ dθ

    =ηk2I2L2

    4π3

    π∫0

    sin3 θ dθ

    ︸ ︷︷ ︸43

    =ηk2I2L2

    3π3

    Since PT =12I

    2Ra, then radiation resistance is solved as

    Ra =2ηk2L2

    3π3

    Interestingly, this is slightly higher than the electrically short monopole. And with noreactive impedance component, this should be easier to match than the short, straightdipole.

    4. Aircraft Communications:

    (a) EIRP = PT + GT (log scale) = 11 dBW

    (b) From logarithmic link budget:

    PR = EIRP +GR − 20 log10(

    λ

    )− 20 log10 r

    where λ = 0.43 m at 700 MHz, r is TR separation distance, GR = 6 dBi, and PR=114dBW. Solving for r gives a range of 158 kilometers.

    (c) There is a mismatch factor of 0.64 on the link (1.9 dB). All else being equal, a receivedpower of -86 dBm now corresponds to a link distance of 120 kilometers, nearly a 20%decrease.

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