发明名称 Method for determining orientation and attitude of a satellite- or aircraft-borne phased-array antenna
摘要 A Tripulse method determines the orientation or attitude of a phased-array antenna located at a remote site, such as an aircraft or spacecraft. Three pulses are transmitted from the phased-array antenna in an estimated direction toward a coherent receiver, with a sum beam, and with first and second difference beams formed by reversal of the phase of certain elements above a first axis of symmetry, and to one side of a second axis of symmetry. The received signals are processed in a manner which determines the error between the assumed direction and the actual direction of the receiver. To determine the rotational position of the array antenna, the same steps are performed for a second remote receiver, and additional processing determines the complete attitude, including yaw, of the phased-array antenna. The coherent receiver may use the first transmitted pulse as a reference, or it may use a separate reference signal.
申请公布号 US5790071(A) 申请公布日期 1998.08.04
申请号 US19970887691 申请日期 1997.07.03
申请人 LOCKHEED MARTIN CORP. 发明人 SILVERSTEIN, SETH DAVID;ASHE, JEFFREY MICHAEL;KAUTZ, GREGORY MICHAEL;WHEELER, FREDERICK WILSON;JACOMB-HOOD, ANTHONY WYKEHAM
分类号 H01Q1/18;H01Q1/28;H01Q3/30;H04B7/185;H04B7/204;(IPC1-7):H04B7/185 主分类号 H01Q1/18
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