Abstract: The present invention is directed to an antenna system. The antenna system may include a first antenna and a second antenna. The antenna system may further include a first LRU connected to the first antenna, and a second LRU connected to the second antenna. The antenna system may further include a router, said router being connected to the first LRU, the second LRU and a communication system, the communication system being remotely located from the antenna system. The router may be configured for receiving a plurality of concurrent (ex.—simultaneous) communication control inputs from the communication system and may selectively route the received communication control inputs to the LRUs. The LRUs may, based upon the received communication control inputs establish LRU settings for causing the antennas to transmit and/or receive communications in accordance with said communication control inputs.

Abstract: The present invention is directed to an avionics system. The avionics system may include a plurality of multi-function antennas. Each multi-function antenna includes a plurality of antenna elements and an antenna electronics system, the antenna electronics system being communicatively coupled with the plurality of antenna elements. The multi-function antennas are configured for being mounted to an exterior surface of a pressure vessel (ex—an exterior surface of an aircraft). The avionics system may further include a plurality of LRUs connected to the antennas via fiber optical cables, the LRUs being located in an interior of the aircraft. The LRUs receive communication control inputs from a communication system and establish settings of the LRUs based upon the received communication control inputs. The multi-function antennas are configured for performing operations (exs.—transmit operations, receive operations) based upon the settings established by the LRUs and based upon the communication control inputs.