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138   Introduction to Space Sciences and Spacecraft Applications

                         range and is measured along the direction in which the sensor is looking
                         (boresight). From the aspect of the point on the earth being viewed, the angle
                         fiom the horizon to the satellite along the boresight is called the elevation (or
                         grazing) angle (w), and the complement of this angle is called the incidence
                         ang2e (ei). The angular distance from the nadir to the point being viewed, as
                         measured from the center of the earth, is called the earth angle (y).
                           Given the altitude of the satellite (h) and any one of the viewing angles,
                         the slant range and all of the other angles can be calculated using:

                           R2 = (h + RJ2 + RZ - 2R, (h + k) COS($                   (6- 1)

                         and the law of sines:
                             R
                                     R
                                              h+R,
                           -=e=
                           sin(y)   si@,)   sin(yl+ 90)
                         Because the sensor may only be looking at a small portion of the available
                         field of  view at any particular time, a description of the area in view and
                         a method of viewing the total area available must be developed.

                         Instantaneous Field of View. Just as a telescope of increasing power sees
                         a smaller area on the face of the moon (for example), many remote sen-
                         sors concentrate on a small portion of the FOV at any particular time. This
                         smaller portion of the FOV visible by the sensor is known as the instanta-
                         neous field of view (IFOV). The remote sensor’s ability to resolve spatial
                         targets within the IFOV depends on the spatial acuity or dimensions of the
                         detector’s  picture element (pixel) or resolution cell which is a characteris-
                         tic of the physical make-up of the sensing device itself.
                           A  passive remote  sensor’s IFOV  is  dependent upon  the  wavelength
                         scaled dimension of  the collection or focusing element (antenna or lens)
                         and the distance from the remote sensor to the target area being observed,
                         as shown by (equation 6-3), sometimes referred to as the diffruction limit
                         of spatial performance.

                           rFov=(;).                                                (6 - 3)


                         where:
                            h = primary wavelength of observation
                           D = dimension of the aperture (lens, antenna, mirror, etc.)
                           R = range from the sensor to the target area
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