For the aircraft in Prob. 4, sketch the approximate unaliased slant rangevelocity distribution of the ground clutter (mainlobe + sidelobe) in a\ birds-eye format similar to that of Fig. 5.36a. The slant range axis of the\ sketch should cover 0 to 100 km and the velocity axis should cover \\\\pm vmax\ ,\ where vmax\ is the maximum possible radial velocity in meter per second\ that could be observed from scatterers in front of the radar. It is not\ necessary to represent antenna gain effects; concentrate on indicating\ where the mainlobe clutter will be centered and the intervals in range and\ velocity where clutter energy will be seen