Practical_Antenna_Handbook_0071639586

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C h a p t e r 3 : A n t e n n a B a s i c s 97 • At the ends of a longer dipole, the current in the dipole must go to zero even though the current at the feedpoint is still I 0 . The contribution to the received signal at a distant point from each short segment of the antenna is then summed at the distant location, taking into account the different propagation times to the receiving antenna from different segments of the source dipole. In this model of a longer dipole, a current introduced at the feedpoint travels along the wire to or from each end. However, at the ends, where no current can flow, a reflection occurs and new currents start back toward the center. We will look at this process in more detail in the next section, but the net effect is that a standing wave of time-varying current (and a similar one for voltage) is created on the wire. This standing wave represents a vector combination of the outbound and returning currents at each point along the dipole. It is the amplitude and phase of this standing wave rather than the individual outbound and returning currents that we use for calculating the contribution of each tiny element of the model to the total radiation detected at a distant point from this dipole. The most common models use either a straight-line decrease of current from the feedpoint to each end or a sinusoidal distribution (again based on reaching zero current at the ends) assuming a source frequency f 0 . The resulting E-field and H-field expressions for longer dipoles are identical to Eqs. (3.19) and (3.20) except for one difference: The sinq term of those equations is now replaced with ⎛ πh ⎞ πh cos cosθ cos ⎝ ⎜ λ ⎠ ⎟ − λ sin θ (3.27) For the special case of the half-wave dipole, Eq. (3.27) reduces to ⎛ π ⎞ π cos cosθ cos ⎝ ⎜ 2 ⎠ ⎟ − 2 sin θ (3.28) Of course, cos (π/2) = cos 90 o = 0, so the second term goes away. Broadside to the axis of the dipole, q = 90o , so the remaining term in the numerator becomes cos 0 o and the entire term has a value of 1.0. Figure 3.7 is a graphical representation of the geometrical variation given by Eq. 3.28—the well-known doughnut pattern of a half-wavelength dipole. When all the approximations are accounted for, the l/2 dipole has 0.4 dB more gain in its main lobe than the hertzian dipole does, and the lobe is slightly narrower than that of the hertzian dipole—but these comparisons are meaningless to everyone except physics professors and their students since it is virtually impossible in the real world to deliver any significant transmitter power to an infinitesimally short dipole! The big news with the l/2 dipole is actually its feedpoint impedance, which in free space is 73 W resistive, with little or no reactive component. This high value of R RAD makes the antenna easy to match with commonly available transmission lines, but, more important, makes it much easier to deliver most of the transmitter output power

98 P a r t I I : F u n d a m e n t a l s C Antenna axis B End view of vertical plane (rotated 90˚ from solid figure) 315 270 A Top view of horizontal plane (rotated 90˚ from solid figure) 0 90 45 Figure 3.7 Free-space radiation pattern of l/2 dipole. to the antenna rather than seeing it dissipate in the resistance of conductors and connectors. Standing Waves Assume that it is possible to have a wire conductor with one end extending infinitely, with a transmitter or other source of RF energy of single frequency f 0 connected to this wire. When the transmitter is turned on, an alternating current consisting of sine waves propagates along the wire. These waves are called traveling waves, and, although the

C h a p t e r 3 : A n t e n n a B a s i c s 97<br />

• At the ends of a longer dipole, the current in the dipole must go to zero even<br />

though the current at the feedpoint is still I 0 .<br />

The contribution to the received signal at a distant point from each short segment of<br />

the antenna is then summed at the distant location, taking into account the different<br />

propagation times to the receiving antenna from different segments of the source dipole.<br />

In this model of a longer dipole, a current introduced at the feedpoint travels along<br />

the wire to or from each end. However, at the ends, where no current can flow, a reflection<br />

occurs and new currents start back toward the center. We will look at this process<br />

in more detail in the next section, but the net effect is that a standing wave of time-varying<br />

current (and a similar one for voltage) is created on the wire. This standing wave<br />

represents a vector combination of the outbound and returning currents at each point<br />

along the dipole. It is the amplitude and phase of this standing wave rather than the<br />

individual outbound and returning currents that we use for calculating the contribution<br />

of each tiny element of the model to the total radiation detected at a distant point<br />

from this dipole.<br />

The most common models use either a straight-line decrease of current from the<br />

feedpoint to each end or a sinusoidal distribution (again based on reaching zero current<br />

at the ends) assuming a source frequency f 0 .<br />

The resulting E-field and H-field expressions for longer dipoles are identical to Eqs.<br />

(3.19) and (3.20) except for one difference: The sinq term of those equations is now replaced<br />

with<br />

⎛ πh<br />

⎞ πh<br />

cos cosθ<br />

cos<br />

⎝<br />

⎜<br />

λ ⎠<br />

⎟ −<br />

λ<br />

sin θ<br />

(3.27)<br />

For the special case of the half-wave dipole, Eq. (3.27) reduces to<br />

⎛ π ⎞ π<br />

cos cosθ<br />

cos<br />

⎝<br />

⎜ 2 ⎠<br />

⎟ − 2<br />

sin θ<br />

(3.28)<br />

Of course, cos (π/2) = cos 90 o = 0, so the second term goes away.<br />

Broadside to the axis of the dipole, q = 90o , so the remaining term in the numerator<br />

becomes cos 0 o and the entire term has a value of 1.0. Figure 3.7 is a graphical representation<br />

of the geometrical variation given by Eq. 3.28—the well-known doughnut pattern<br />

of a half-wavelength dipole. When all the approximations are accounted for, the<br />

l/2 dipole has 0.4 dB more gain in its main lobe than the hertzian dipole does, and the<br />

lobe is slightly narrower than that of the hertzian dipole—but these comparisons are<br />

meaningless to everyone except physics professors and their students since it is virtually<br />

impossible in the real world to deliver any significant transmitter power to an infinitesimally<br />

short dipole!<br />

The big news with the l/2 dipole is actually its feedpoint impedance, which in free<br />

space is 73 W resistive, with little or no reactive component. This high value of R RAD<br />

makes the antenna easy to match with commonly available transmission lines, but,<br />

more important, makes it much easier to deliver most of the transmitter output power

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