Vis enkel innførsel

dc.contributor.authorMerz, Mariann
dc.contributor.authorJohansen, Tor Arne
dc.date.accessioned2019-11-25T11:21:32Z
dc.date.available2019-11-25T11:21:32Z
dc.date.created2019-11-23T14:49:35Z
dc.date.issued2019
dc.identifier.issn0731-5090
dc.identifier.urihttp://hdl.handle.net/11250/2630234
dc.description.abstractThe melting of the Arctic ice cap leads to increased commercial interest in these maritime regions, such as shipping via the Northeast Passage and oil and gas exploration, leading to a need to develop new long-range unmanned technologies to support operations as well as to provide solutions for environmental monitoring. This Note attempts to support this development by adding to the capabilities of fixed-wing unmanned aerial vehicles (UAVs) such that they can support new types of long-range missions. Circular towing, where a cable with an attached end body is towed behind a UAV that tracks a circular path, is looked into as a way to facilitate high-precision gentle object placement of instruments/equipment that are sensitive to gravity forces, and potentially to manipulate or retrieve small objects. Furthermore, the method may be used for missions that require the towed end body to move at speeds much lower than the minimum UAV speed (potentially interesting for various surveillance and tracking applications). Although many research efforts have established that an optimally configured steady-state circular-towing scenario in the absence of wind and disturbances yields an end body that is stabilized in a low-speed small radius orbit relative to a point on the ground [1–5], the challenging operating conditions in the Arctic and maritime environments demand a design that is robust to moderate wind levels and to gradual variations in wind magnitude and direction. The effect of wind on the aerially towed system was analyzed in Refs. [3,6–9] in various levels of detail, but the achievable end body precision in winds for a small UAV towed system cannot be derived from any of these studies due to significant differences in towed system size or application.nb_NO
dc.language.isoengnb_NO
dc.publisherAmerican Institute of Aeronautics and Astronauticsnb_NO
dc.titleControl of an End Body Towed by a Circling Unmanned Aerial Vehiclenb_NO
dc.typeJournal articlenb_NO
dc.typePeer reviewednb_NO
dc.description.versionacceptedVersionnb_NO
dc.source.journalJournal of Guidance Control and Dynamicsnb_NO
dc.identifier.doi10.2514/1.G004199
dc.identifier.cristin1751339
dc.relation.projectNorges forskningsråd: 223254nb_NO
dc.description.localcode© 2019. This is the authors' accepted and refereed manuscript to the article. The final authenticated version is available online at: http://dx.doi.org/10.2514/1.G004199nb_NO
cristin.unitcode194,63,25,0
cristin.unitnameInstitutt for teknisk kybernetikk
cristin.ispublishedtrue
cristin.fulltextpostprint
cristin.qualitycode1


Tilhørende fil(er)

Thumbnail

Denne innførselen finnes i følgende samling(er)

Vis enkel innførsel