Emergency aircraft landing systems and methods
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United States of America Patent
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Jun 28, 2016
Grant Date -
Jun 21, 2012
app pub date -
Dec 20, 2010
filing date -
Dec 20, 2010
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Abstract
Emergency aircraft landing systems and methods are described. In one aspect, an emergency landing apparatus includes a support structure for a fuselage and wings of an aircraft and a control system. The control system includes a processor and a memory containing computer program instructions executable by the processor. Execution of the computer program instructions causes an interface on the aircraft to exchange information between an aircraft guidance and control system on the aircraft and the control system. The computer program instructions further synchronize the speed and position of the emergency aircraft landing apparatus on a runway with the speed and flight path of the aircraft.
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