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dc.contributor.authorYakimenko, O.
dc.contributor.authorDobrokhodov, V.
dc.contributor.authorJohnson, J.
dc.contributor.authorKaminer, I.
dc.contributor.authorDelliker, S.
dc.contributor.authorBenney, R.
dc.date2002
dc.date.accessioned2016-12-08T16:38:01Z
dc.date.available2016-12-08T16:38:01Z
dc.date.issued2002
dc.identifier.citation15th Triennial World Congress, Barcelona, Spainen_US
dc.identifier.urihttp://hdl.handle.net/10945/50773
dc.description.abstractThis paper addresses the development of an autonomous guidance, navigation and control system for a flat solid circular parachute. This effort is a part of the Affordable Guided Airdrop System (AGAS) that integrates a low-cost guidance and control system into fielded cargo air delivery systems. The paper describes the AGAS concept, its architecture and components. It further proceeds with the description of the control strategy based on Pontrjagin’s principle of optimality. The paper ends with the results of the final AGAS demonstration performed at the U.S. Army Yuma Proving Ground in September, 2001.en_US
dc.format.extent6 p.en_US
dc.publisherIFACen_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.titleGuidance and control of affordable guided airdrop systemen_US
dc.typeConference Paperen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)en_US
dc.subject.authorautomated guided vehiclesen_US
dc.subject.authoroptimal controlen_US
dc.subject.authorflight controlen_US


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