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236                                                       ANTENNA BASICS


                                  2 2
                                   
        back to radar receiver  =  3   . Here  = () is the radar antenna gain. If so, the
                                      
                            
                                              
                               �4 �  4
        power supplied to radar receiver
                                  2 2        4 2           2
                                            
                        () =  3   =  3   =  3  >   ∆        (5.71)
                                                                     
                                                                  
                                     
                                                   
                        
                                              4 4
                                                            4
                               �4 �  4  �4 �     �4 �  
        would be maintained constant and exceeds the noise level for any target at a distance  <   .
        In other words, the squared pattern is a means of achieving a more uniform signal strength at
        the input of the receiver. Since the elevation angle , distance r and h are related as  cos =
                                    2
                               2
                                                  2
                                              2
                                         2
        ℎ/,  we can  write ()~ = ℎ ⁄ cos  = ℎ csc   where  ℎ = .  If  so, the pattern
        envelope should remind (black curve in Figure 5.4.1e) the graph of function csc.
        The last example in Figure 5.4.1f demonstrates the pattern of an antenna emitting a so-called
        contour beam. Antennas with such a beam are typically an integral part of communication
        satellites placed in Geostationary Orbit (GEO) [15] at an altitude of about 35,786 km (22,236
        miles) directly over the Earth’s equator. Since the rotation period of these satellites and Earth
        are the same their position over the Earth’s equator is almost permanent (with slight deviations).
        Therefore, they can serve as motionless space relay stations bouncing communication and/or
        broadcast signals  from the Earth back to different geographical regions called
                                   22
        satellite's footprints. Figure 5.4.2a  illustrates the principle of footprint formation while Figure
        5.4.2b displays the one of Astra 4A  [14] footprint covering most of Europe. Here the numbers
        attached to contour curves indicate the constant EIRP in dBW (look back at Section 5.3.2).







             a)                                 b)



            Figure 5.4.2 a) Illustration of satellite’s footprint establishment, b) Astra 4A satellite
                                          footprint
        5.4.2  Basics of Linear Array Analysis

        In Section 4.2 of Chapter 2, we have considered several types of antennas defined as elementary
        radiators.  In common,  they have  broad  radiation  patterns  of  simple shape and  consequently
        relatively low directivity (gain). It means they certainly do not meet the requirements for long
        distance  communications,  radars  and  most  other  systems  discussed  in  Section  5.3  of
        this chapter. Furthermore, none of elementary radiators is able to form the patterns shown in
        Figure 5.4.1 (except depicted in Figure 5.4.1a) where antennas with high directivity are
        required.  We  can  obtain  some  preliminary  guidance  from  equations  (4.72)  and  (4.85)


        22  Public Domain Image, source: http://www.its.bldrdoc.gov/fs-1037/dir-016/_2287.htm
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