By distributing antenna elements or small subarrays throughout the skin of an aircraft, a large portion of the airframe can act as an electromagnetic transducer. The basic problem associated with such a design is that uncertainties in element locations due to the nonrigidness of the airframe induce phase errors. Self-cohering techniques are required to compensate for those errors. Four such techniques are presented here.
Self-Cohering an Airborne e Radio Camera
IEEE Transactions on Aerospace and Electronic Systems ; AES-19 , 3 ; 483-490
1983-05-01
1852340 byte
Article (Journal)
Electronic Resource
English
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