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Unit 8: Space Wave Propagation
Dr. P C Srikanth
Professor and Former Head
24-1 Introduction
• Figure 24-1 shows the attenuation of ground waves for good and
poor earth.
• It can be seen from these figures that with the increase of
frequency, the rate of attenuation increases.
• The signal strength in case of poor earth reduces to the same level
in 800 km for 1MHz and a little over 200 km for 10MHz.
• From Fig. 24-2, it can be seen that the energy contents of space-
wave travel from transmitter to receiver partly through direct wave
(DW) or direct ray (DR) and partly through the reflected wave (RW)
or reflected ray (RR).
• In this figure, the earth curvature is neglected for simplifying the
illustration and the analysis.
• The net field strength at the receiving antenna will be the vector
sum of DW and RW fields.
24-1 Introduction
24-1 Introduction
24-2 Field Strength Relation
• When the distance (d) between transmitting and
receiving antennas is sufficiently large in comparison to
antenna heights (ht and hr), the incidence angle ψ of
the ray on earth is small.
• In view of Fig. 24-3, reflection from earth, irrespective
of polarisation, can be assumed to have no change in
magnitude but with reversal of phase.
• Thus the two waves arriving at the receiver will have
equal amplitudes but different phases.
• Assuming E0 to be the amplitude of DW and RW at a
unit distance at a distance d, the amplitudes of both
(DW and RW) reduce to E´=E0/d.
24-2 Field Strength Relation
• Figure 24-4(a), a modified version of Dig. 24-2, illustrates
different parameters.
• These include the transmitting antenna T located at A, with
height ht, receiving antennas located at B with height hr , R1
the distance travelled by DW, R2 the distance travelled by
RW both between T and R and the angle-ψ.
• The R2 shown is the distance between T and R via O, i.e.,
the point from where the wave reflects.
• Alternatively, it is the distance travelled by RR from T* to R
where T* is the image of the transmitting antenna.
• The resultant field E can now be obtained from Fig. 24-4(a
and b) as below.
24-2 Field Strength Relation
• R1² = (ht-hr)²+d² ..........1
• R2² = (ht+hr)²+d² ..........2
• R1 = d[1+(ht-hr)²/2d²] .......3
• R2 = d[1+ (ht+hr)²/ 2d²] .......4
• The difference in path lengths R2 and R1 is obtained to be
• R2 - R1 = [(ht+hr)² - (ht-hr)²] / 2d² = 2hthr / d ....5
• The phase difference corresponding to this path differences is
• (2π/λ) (2hthr ) / d = (4πhthr)λd radians .......6
• E = (2E0/d) sin [(2πhthr ) / λd] ........7
• When [(2πhthr ) / λd] is less than 0.5, the sine of the angle can be
replaced by the angle itself and thus 7 reduces to,
• E = (2E0/d) [(2πhthr ) / λd] = [(4πhthr)/λd²] E0 .........8
24-2 Field Strength Relation
24-2 Field Strength Relation
24-3 Effects of Imperfect Earth
• In Fig. 24-5 (a), d´ is the distance at which free space field and
oscillating field for a perfectly conducting earth become equal.
• It is less than the value that makes the angle [(2πhthr) /λd] greater
than λ/6.
• It can be observed that the field strength oscillates about the value
E0 / d, which corresponds to the strength of the direct ray.
• For a perfectly conducting earth, the maximum amplitude of these
oscillation is twice of the free-space value.
• For d˃d’ , path lengths of DW and RW always differ by less than λ/6,
in such cases E falls rapidly in accordance with the proportionality
with distance square.
• For d˃d’ , the angle of incidence is so small that reflection takes
place with the reversal of phase and no change in amplitude for
both polarizations.
• The resulting field will be less than the free space values.
24-3 Effects of Imperfect Earth
24-3 Effects of Curvature of Earth
• Due to curvature of earth :
• The effective and actual antenna heights shown in Fig. 24-6 differ.
• The quantum of difference will depend on the separation between
Tx and Rx.
• There is a change in the number and location of maximas and
minimas as illustrated in Fig. 24-5.
• There is reduction in d’, beyond which the two waves tend to be out
of phase.
• At large distances, for small incidence angles and DW and RW in
phase opposition, the resultant E at Rx is apparently greater than
that if earth were flat.
• The last two effects of curvature try to neutralize each other.
24-3 Effects of Curvature of Earth

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Space Wave Propagation Fundamentals

  • 1. Unit 8: Space Wave Propagation Dr. P C Srikanth Professor and Former Head
  • 2. 24-1 Introduction • Figure 24-1 shows the attenuation of ground waves for good and poor earth. • It can be seen from these figures that with the increase of frequency, the rate of attenuation increases. • The signal strength in case of poor earth reduces to the same level in 800 km for 1MHz and a little over 200 km for 10MHz. • From Fig. 24-2, it can be seen that the energy contents of space- wave travel from transmitter to receiver partly through direct wave (DW) or direct ray (DR) and partly through the reflected wave (RW) or reflected ray (RR). • In this figure, the earth curvature is neglected for simplifying the illustration and the analysis. • The net field strength at the receiving antenna will be the vector sum of DW and RW fields.
  • 5. 24-2 Field Strength Relation • When the distance (d) between transmitting and receiving antennas is sufficiently large in comparison to antenna heights (ht and hr), the incidence angle ψ of the ray on earth is small. • In view of Fig. 24-3, reflection from earth, irrespective of polarisation, can be assumed to have no change in magnitude but with reversal of phase. • Thus the two waves arriving at the receiver will have equal amplitudes but different phases. • Assuming E0 to be the amplitude of DW and RW at a unit distance at a distance d, the amplitudes of both (DW and RW) reduce to E´=E0/d.
  • 6. 24-2 Field Strength Relation • Figure 24-4(a), a modified version of Dig. 24-2, illustrates different parameters. • These include the transmitting antenna T located at A, with height ht, receiving antennas located at B with height hr , R1 the distance travelled by DW, R2 the distance travelled by RW both between T and R and the angle-ψ. • The R2 shown is the distance between T and R via O, i.e., the point from where the wave reflects. • Alternatively, it is the distance travelled by RR from T* to R where T* is the image of the transmitting antenna. • The resultant field E can now be obtained from Fig. 24-4(a and b) as below.
  • 7. 24-2 Field Strength Relation • R1² = (ht-hr)²+d² ..........1 • R2² = (ht+hr)²+d² ..........2 • R1 = d[1+(ht-hr)²/2d²] .......3 • R2 = d[1+ (ht+hr)²/ 2d²] .......4 • The difference in path lengths R2 and R1 is obtained to be • R2 - R1 = [(ht+hr)² - (ht-hr)²] / 2d² = 2hthr / d ....5 • The phase difference corresponding to this path differences is • (2π/λ) (2hthr ) / d = (4πhthr)λd radians .......6 • E = (2E0/d) sin [(2πhthr ) / λd] ........7 • When [(2πhthr ) / λd] is less than 0.5, the sine of the angle can be replaced by the angle itself and thus 7 reduces to, • E = (2E0/d) [(2πhthr ) / λd] = [(4πhthr)/λd²] E0 .........8
  • 10. 24-3 Effects of Imperfect Earth • In Fig. 24-5 (a), d´ is the distance at which free space field and oscillating field for a perfectly conducting earth become equal. • It is less than the value that makes the angle [(2πhthr) /λd] greater than λ/6. • It can be observed that the field strength oscillates about the value E0 / d, which corresponds to the strength of the direct ray. • For a perfectly conducting earth, the maximum amplitude of these oscillation is twice of the free-space value. • For d˃d’ , path lengths of DW and RW always differ by less than λ/6, in such cases E falls rapidly in accordance with the proportionality with distance square. • For d˃d’ , the angle of incidence is so small that reflection takes place with the reversal of phase and no change in amplitude for both polarizations. • The resulting field will be less than the free space values.
  • 11. 24-3 Effects of Imperfect Earth
  • 12. 24-3 Effects of Curvature of Earth • Due to curvature of earth : • The effective and actual antenna heights shown in Fig. 24-6 differ. • The quantum of difference will depend on the separation between Tx and Rx. • There is a change in the number and location of maximas and minimas as illustrated in Fig. 24-5. • There is reduction in d’, beyond which the two waves tend to be out of phase. • At large distances, for small incidence angles and DW and RW in phase opposition, the resultant E at Rx is apparently greater than that if earth were flat. • The last two effects of curvature try to neutralize each other.
  • 13. 24-3 Effects of Curvature of Earth