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Ionospheric Phase Shift

[a] Show that the phase shift of a radiation field over any path can be written:

displaymath850

where n(s) is the phase refractive index along the path.
Note then, that if the path changes continuously with time (due say to the source of the radiation moving), there will be a doppler shift:

displaymath851

imposed on the signal which depends on the properties of the medium. Measurement of this doppler shift could, in principle, be used to measure properties of the medium.

SOLUTION:

Since the phase shift must be tex2html_wrap_inline902 for every wavelength:

displaymath852

displaymath853

where tex2html_wrap_inline904 is the vacuum wavelength.

Under the circumstances we discuss here:

displaymath854

The frequency shift will then be:

displaymath855

The first term in the integral gives the vacuum Doppler shift:

displaymath856

Where tex2html_wrap_inline906 is the satellite radial velocity toward the observer.

The ionospheric plasma `doppler shift' is much smaller:

displaymath857

Since the maximum value of X is about tex2html_wrap_inline910 .

(We can get at tex2html_wrap_inline912 from tex2html_wrap_inline914

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[b] An artificial Earth satellite is in circular orbit 1000km above the Earth's surface. It transmits a 200MHz radio signal. At some instant, the line of sight makes an angle of tex2html_wrap_inline666 to the vertical for an observer on Earth who is in the plane of the satellite orbit.

At such a high frequency we can show that the effects of the ionospheric plasma on the radio wave are very weak (i.e. the deviation of the refractive index from unity is very small). Consequently, the effect of the plasma on the phase of the signal can be computed using the simplest theoretical expression, neglecting the magnetic field:

displaymath858

Show that the doppler shift seen by this observer consists of:

SOLUTION:
Using a flat Earth approximation, if the zenith angle of the satellite is tex2html_wrap_inline666 , the satellite radial velocity is tex2html_wrap_inline926 where v is the speed of the satellite in its circular path around the Earth. We can calculate v using Newtonian gravity. If R is the radius of the Earth and h is the height of the satellite above theEarth and M is the Earth mass:

displaymath859

Using h=1000km, tex2html_wrap_inline940 , tex2html_wrap_inline942 , tex2html_wrap_inline944 :

displaymath860

The vacuum doppler shift would be:

displaymath861

Since the vacuum wavelength at 200MHz is 1.5m.
The ionospheric doppler shift:

displaymath862

A more precise estimate of tex2html_wrap_inline948 :
From above the magnitude of the ionospheric phase shift is:

displaymath863

Putting tex2html_wrap_inline950 (where tex2html_wrap_inline952 is the zenith angle of the satellite):

displaymath864

Assuming the ionosphere is horizontally stratified so tex2html_wrap_inline954 does not change with time:

displaymath865

displaymath866

displaymath867

Using tex2html_wrap_inline956 :

displaymath868

tex2html_wrap_inline958 would be a typical daytime value for tex2html_wrap_inline960 so:

displaymath869

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[c] Clearly the ionospheric doppler shift would be hard to measure in the presence of the much larger vacuum doppler shift.
Show that the ionospheric doppler shift can be separated out if the satellite simultaneously coherently emits a harmonic of the 200MHz.
Show that this could lead to a measurement of the integrated electron concentration along the path from the satellite to the observer.

SOLUTION:

In general:

displaymath870

So for the fundamental frequency (200MHz in this case):

displaymath871

For the nth harmonic, tex2html_wrap_inline966 and tex2html_wrap_inline968 .

displaymath872

So to subtract out the vacuum doppler contributions and leave the ionospheric doppler shift we need to divide the nth harmonic by n and subtract (in a mixer circuit).

displaymath873

displaymath874

Note that the process of subtracting out the vacuum doppler shift does not completely subtract out the ionospheric doppler shift because it has a different frequency dependence from the vacuum effect.


next up previous
Next: About this document Up: No Title Previous: Distance to Taurus A

Keith Jones
Fri Mar 24 09:38:47 EST 2000