发明名称 Aircraft emergency safety control system, method and apparatus
摘要 A system capable of regaining control of an aircraft (120a, 120b, 120c) that may have been lost due to incapacitation of the crew includes an airborne segment on the aircraft (120), a ground segment (130a, 130b, 130c) and a communications segment (10) wherein control of the aircraft (120) is removed from the control of unauthorised person(s) onboard the aircraft (120), and the aircraft is directed to a destination that is considered a safe location for the aircraft given its status, and to facilitate a reasonably safe emergency landing. The ground segment comprises monitoring and control equipment (130a, 130b, 130c) capable of monitoring the aircraft (120) and determining the presence of an emergency situation onboard the aircraft. The airborne segment comprises a navigational system capable of providing autonomous control of the aircraft (120) upon receipt of a signal from the ground segment (130a, 130b, 130c). <IMAGE>
申请公布号 EP1422680(A2) 申请公布日期 2004.05.26
申请号 EP20030256137 申请日期 2003.09.29
申请人 RAYTHEON COMPANY 发明人 LANGSTON, JAMES LELAND
分类号 B64D45/00;G08G5/00;(IPC1-7):G08G5/00 主分类号 B64D45/00
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