Page 119 - Satellite Communications, Fourth Edition
P. 119

The Geostationary Orbit  99

                              3.9 Problems

                              3.1.  Explain what is meant by the geostationary orbit. How do the
                              geostationary orbit and a geosynchronous orbit differ?

                              3.2.  (a) Explain why there is only one geostationary orbit. (b) Show that the
                              range d from an earth station to a geostationary satellite is given by
                                                          2
                                              d   2sR sin Eld   hs2R   hd   R sin El,
                              where  R  is the earth’s radius (assumed spherical),  h  is the height of the
                              geostationary orbit above the equator, and El is the elevation angle of the earth
                              station antenna.
                              3.3.  Determine the latitude and longitude of the farthest north earth station
                              which can link with any given geostationary satellite. The longitude should be
                              given relative to the satellite longitude, and a minimum elevation angle of 5°
                              should be assumed for the earth station antenna. A spherical earth of mean
                              radius 6371 km may be assumed.

                              3.4.  An earth station at latitude 30°S is in communication with an earth
                              station on the same longitude at 30°N, through a geostationary satellite. The
                              satellite longitude is 20° east of the earth stations. Calculate the antenna-look
                              angles for each earth station and the round-trip time, assuming this consists of
                              propagation delay only.

                              3.5. Determine the maximum possible longitudinal separation which can exist
                              between a geostationary satellite and an earth station while maintaining line-
                              of-sight communications, assuming the minimum angle of elevation of the earth
                              station antenna is 5°. State also the latitude of the earth station.

                              3.6. An earth station is located at latitude 35°N and longitude 100°W. Calculate
                              the antenna-look angles for a satellite at 67°W.

                              3.7. An earth station is located at latitude 12°S and longitude 52°W. Calculate
                              the antenna-look angles for a satellite at 70°W.

                              3.8. An earth station is located at latitude 35°N and longitude 65°E. Calculate
                              the antenna-look angles for a satellite at 19°E.

                              3.9. An earth station is located at latitude 30°S and longitude 130°E. Calculate
                              the antenna-look angles for a satellite at 156°E.

                              3.10. Calculate for your home location the look angles required to receive from
                              the satellite (a) immediately east and (b) immediately west of your longitude.
                              3.11.  CONUS is the acronym used for the 48 contiguous states. Allowing for
                              a 5° elevation angle at earth stations, verify that the geostationary arc required
                              to cover CONUS is 55° to 136°W.
   114   115   116   117   118   119   120   121   122   123   124