Abstract: The line of sight of an airborne radar antenna is stabilized from the pitch and roll motions of the aircraft by mounting the antenna on a three degree of freedom gimbal system. The gimbal system is comprised of a first gimbal mounted for rotation about the aircraft Z axis (azimuth) for pointing the antenna along the intended line of sight, a second gimbal mounted on the first gimbal for rotating up and down with respect to the azimuth gimbal and a third gimbal mounted on the second gimbal to which the antenna is connected for providing rotation to align antenna polarization relative to inertial ground. A two degree of freedom stabilization gyro provides stabilizing signals representative of aircraft pitch and roll motions with respect to inertial reference axes.

Abstract: An apparatus and method for forming an antenna reflector panel to a desired shape. The apparatus includes a plate having a plurality of threaded holes, wherein a threaded stud is located in each one of the plurality of threaded holes. The tops of the threaded studs define the desired antenna panel contour. Two metal sheets with a honeycomb structure between them are urged against the stud tops by enclosing the fixture and drawing a vacuum therein. After the metal sheets and honeycomb structure have been held in the desired contour for a predetermined time the vacuum is released. The sheet and honeycomb structure are now permanently deformed into the desired shape.