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Astronomy Principles and Practice Fourth Edition.pdf

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Observational radio astronomy 427<br />

via the formula<br />

cos φ = cos2 α max + (R 2 − cos 2 α max ) 1/2 sin α max<br />

. (24.6)<br />

R<br />

It will also be appreciated that for a satellite to be on the observer’s meridian (i.e. with azimuth<br />

A = 180 ◦ ), its longitude value must match that of the observer’s longitude.<br />

Thus, from measurements of the azimuth <strong>and</strong> altitude of a number of satellites, it is possible to<br />

determine the latitude <strong>and</strong> longitude of the observing station. In order to achieve this with reasonable<br />

accuracy, the measurements of the satellite positions should be made to an accuracy of about ±1/2 ◦ .<br />

Table 24.1 gives a list of some of the geostationary satellites presently in orbit according to their<br />

longitudes about the Greenwich meridian, with a guide as to their relative signal strengths.<br />

Table 24.1. Longitudes of geostationary communication satellites visible from Glasgow (λ s − ve is E, λ s + ve<br />

is W).<br />

Name Strength λ s Name Strength λ s<br />

Eutelsat II f1 ** −48·0 Intelsat 707 * +1·0<br />

Eutelsat Sesat W4 ** −36·0 Telecom 2B * +5·0<br />

Astra 2A II f1 **** −28·2 Telecom 2A ** +8·0<br />

Kopernikus 3 ** −23·5 Eutelsat IIf2 ** +12·5<br />

Eutelsat II f3 ** −21·5 Telstar 12 *** +15·0<br />

ASTRA **** −19·2 Intelsat 705 * +18·0<br />

Eutelsat W2 ** −16·0 NSSK ** +21·5<br />

Hot Bird *** −13·0 Intelsat 605 ** +27·5<br />

Eutelsat II f4 ** −10·0 Hispasat ** +30·0<br />

Eutelsat W3 ** −7·0 Intelsat 801 * +31·5<br />

Sirius ** −5·0 Intelsat 601 * +34·5<br />

Telecom 2C II f1 ** −3·0 Telstar 11 ** +37·5<br />

Thor ** +0·8 Panamasat 3R ** +43·0<br />

Having set up the simple radio telescope, commence by finding the brightest satellite in the sky—<br />

ASTRA. It should be found at an azimuth of about 150 ◦ . Keep adjusting the sensitivity setting of the<br />

power meter to read mid-scale <strong>and</strong> ‘home-in’ on the satellite position in both altitude <strong>and</strong> azimuth. It<br />

should be possible to estimate the measured angles to about 0·2 ◦ . Note the two values.<br />

Next, adjust the telescope to search for another satellite, Thor. This should be found at an azimuth<br />

of about 150 ◦ . Again home-in on its position <strong>and</strong> record its altitude <strong>and</strong> azimuth.<br />

The altitude of the celestial equator changes only slowly with azimuth at a station with high<br />

latitude, so that the altitude of all the satellites should be fairly similar (within 10 ◦ ). Similarly, the<br />

azimuthal angle between two satellites should be similar to their difference in longitude. Work your<br />

way onto other satellites, noting down their positions. Try to find at least six satellites.<br />

With the data, construct a graph of satellite altitude, a, against satellite azimuth, A. Draw a smooth<br />

curve through the points <strong>and</strong> determine a value for α max corresponding to an azimuth of 180 ◦ . Estimate<br />

how well the value has been determined. Together with the value for R as calculated in equation (24.5),<br />

insert the value of α max in equation (24.6) to determine the latitude of the observing station. Make an<br />

estimate for the uncertainty in the determination by trial adjustments of the value of α max according to<br />

the estimate of its accuracy.<br />

Plot also the satellite longitudes against the measured satellite azimuths. From this graph, estimate<br />

the longitude a satellite would have if it were on the site’s meridian (i.e. if it had an azimuth of<br />

180 ◦ ) <strong>and</strong>, hence, determine the longitude of the observing station. Again, make an estimate for the<br />

uncertainty of this determination.

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