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dc.contributor.authorOleg Yakimenko
dc.contributor.authorCharles HeWgley
dc.contributor.authorEugene Bourakov
dc.date.accessioned2013-10-29T17:35:15Z
dc.date.available2013-10-29T17:35:15Z
dc.date.issued2013-07-09
dc.identifierUS 8,483,891 B2
dc.identifier.urihttp://hdl.handle.net/10945/37052
dc.description.abstractA method is described performing the following. With a parafoil's control unit composed of electronic circuitry, While the control unit is being transported. With a parafoil: calculating a desired landing location for a parafoil, the desired land ing location corresponding to a moving target, the calculating including using a term representative of the moving target’s velocity; determining a flight path to the desired landing location; and, controlling the parafoil’s flight path so as to follow the flight path.en_US
dc.language.isoen_US
dc.publisherThe United States of America as represented by the Secretary of the Navy, Washington, DC (US)en_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleAutomatically Guided Parafoil Directed to Land on a Moving Targeten_US
dc.typePatenten_US
dc.subject.authorPatenten_US


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