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aperture illumination                                         approximation, four-thirds earth radius  41



           ter in the y-z (azimuth) plane. A(z) is a complex function, hav-  While the physical shape of a reflector or lens antenna
           ing both amplitude and phase:                        may be rectangular, the aperture distribution (illumination)
                           A(z) = |A(z)| exp jY(z)              function produced by a feed horn generally has an elliptical
           where |A(z)| = illumination amplitude and Y(z) = illumination  shape, leading to beamwidths and sidelobe levels that are bet-
           phase. At an angle f, the contributions from a particular point  ter predicted as resulting from an elliptical aperture. DKB
           on the aperture will be advanced or retarded in phase by 2p(z/  Ref.: Johnson (1993), p. 2.19.
           l)sinf radians. Each of these contributions is weighted by the
                                                                A synthetic aperture is created by taking advantage of the
           factor A(z). The field intensity is the integral of these individ-
                                                                motion of  a  radar platform to extend  the effective  antenna
           ual contributions across the face of the aperture.
                                                                aperture beyond the limits of its actual physical dimensions.
               For a given field intensity pattern, E(f), the aperture illu-
                                                                In a side-looking synthetic aperture radar (SAR), the effective
           mination can be found from
                                                                beamwidth of the  radar is no longer described by conven-
                           ¥                                    tional (real) antenna relationship  q  =  K l/D, where  the
                          1        æ  2pz    ö                                                3    q
                    Az () ---  ò E f() exp – j --------- sin f dsin f  beamwidth constant K  » 1 depends on aperture weighting,
                        =
                                                                                  q
                          l        è   l     ø
                                                                                e
                           – ¥                                  but by q = K ¢l/L , where L  is the effective length of the
                                                                                        e
                                                                       s
                                                                            q
           which may be used as the basis for synthesizing an antenna  aperture and K ¢ » 0.5. Narrowing of the beamwidth in a syn-
                                                                            q
           pattern, or finding the aperture illumination that yields  the  thetic aperture radar is subject  to certain fundamental  con-
           desired antenna pattern E(f).                        straints: (1) the length L  can be no longer than the width of
                                                                                    e
               Maximum antenna gain and  minimum beamwidth are  the region illuminated by the real aperture: L  £ Rq , and (2)
                                                                                                          3
                                                                                                    e
           realized with a uniform aperture illumination; i.e., one that is  L £ (Rl) 1/2 . The second limitation applies to an unfocused
                                                                 e
           constant  over the aperture and zero everywhere else. Such  SAR,  where the aperture size  must be such that  the phase
           illumination  will  lead to an antenna pattern of the (sin x)/x  front can be considered a plane wave. This limitation can be
           form, with the intensity of the first sidelobe 13.3 dB below  removed in a focused SAR by compensating for the curvature
           peak gain. There exists a large variety of useful illumination  of the spherical wavefront (i.e., applying a phase correction at
           functions, and low sidelobes can be obtained by using func-  each “element”  of the  synthetic  array). See  RADAR, syn-
           tions such as a cosine or a Taylor function. Antennas with the  thetic aperture; ANTENNA, synthetic aperture. PCH
           lowest sidelobes are those  with illumination  functions for  Ref.: Skolnik (1980), Ch. 7; Skolnik (1990), Ch. 6
           which the amplitude tapers  to a small value at the aperture
                                                                aperture tapering (see aperture illumination).
           edges. Lower sidelobes are produced with greater amplitude
           tapering, but at the expense of a wider mainbeam width and  APPROXIMATION
           lower mainbeam gain. Controlling the antenna pattern in this
                                                                detection probability approximation (see  DETECTION
           way is referred to as  aperture tapering.  A table describing
                                                                   probability).
           many of the functions commonly used, and listing the side-
           lobe levels, beamwidth factors, and efficiencies, is given in  The flat-earth approximation  is applicable to very-short-
           the article on  WEIGHTING. Some typical  illumination  range targets in height finding, giving a sufficiently good esti-
           functions  are given in Table W3. (see  also  PATTERN,  mate of target height as
           antenna). PCH, SAL
                                                                                   h =  h +  Rsin q
           Ref.: Skolnik (1990), p. 7.37.                                           t   r      t
                                                                where h  is the radar antenna height, R is the measured target
           aperture illumination efficiency (see antenna directivity).  a
                                                                range, q is the measured or estimated target elevation angle,
                                                                       t
           aperture matching (see ARRAY aperture matching).     and h  is the estimated target height. SAL
                                                                    t
           A passive aperture is one that focuses energy received from  Ref.: Skolnik (1990), p. 20.14.
           a true  source outside the antenna  (as  opposed to an active  The four-thirds earth radius approximation expresses the
           aperture).                                           refractive effects of the troposphere in terms of straight ray
                                                                paths over a spherical earth whose radius is ka, where k = 4/3
           A  rectangular aperture consists  of rows and columns of
                                                                              6
                                                                and a = 6.5 ´ 10  is the true radius of the earth (see ATMO-
           radiating elements  with an aperture illumination defined
                                                                SPHERE, refraction). The refractive index implied by this
           along those coordinates. The beamwidth of a uniformly illu-
                                                                model varies linearly in the lower atmosphere:
           minated rectangular aperture of width w is q = 0.886l/w, and
                                              3
           the sidelobe level is -13.3 dB. In many cases, the illumination
           functions in the x-and y-coordinates are separable:                    nh () n –=  0  k h
                                                                                             1
                                   =
                             gx y ,(  ) gx () gy ()
                                                                where n  » 1.000313 is the refractive index of the atmosphere
                                                                      0
           In that case, the antenna patterns in each coordinate may be                 - 8
                                                                at the surface and k  » 4 ´ 10  per meter is the assumed gra-
                                                                                1
           calculated separately, each being the Fourier transform of the
                                                                dient of refractive index with respect to height, h. In general,
           corresponding illumination function.
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