发明名称 Refueling boom control system
摘要 A method and apparatus comprising a refueling controller (426). The refueling controller (426) is configured to receive a number of operator commands (424) for moving a refueling boom (412) on a tanker aircraft (408) in a desired direction. The number of operator commands (424) defines at least one of an azimuth movement (476) and an elevation movement (478) of the refueling boom (412) during flight of the tanker aircraft (408). The refueling controller (426) is further configured to generate a number of intermediate commands (458) for moving the refueling boom (412) in the desired direction as defined by the number of operator commands (424). The number of intermediate commands (458) defines at least one of a roll movement (480) and a pitch movement (482) such that the refueling boom (412) moves in the desired direction.
申请公布号 AU2013206363(B2) 申请公布日期 2017.03.23
申请号 AU20130206363 申请日期 2013.06.17
申请人 The Boeing Company 发明人 Hatcher, Justin Cleve;Speer, Thomas Edward;Musgrave, Jeffrey L.
分类号 B64D39/04;B64D3/00;B64D39/00;G01S5/00 主分类号 B64D39/04
代理机构 代理人
主权项
地址