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Flight Formation Control > urlin.us/3pxsz

























































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of Electr. Castro ; R. JavaScript is disabled on your browser. Cookies are required to use this site. Enter Search Term First Name / Given Name Family Name / Last Name / Surname Publication Title Volume Issue Start Page Search Basic Search Author Search Publication Search Advanced Search Other Search Options Command Search Citation Search Search Alerts Search History . For more information, visit the cookies page.Copyright 2016 Elsevier B.V.

Lozano Abstract Authors References Cited By Keywords Metrics Similar Download Citation Email Print Request Permissions In this paper it is presented a control strategy to solve the trajectory tracking and flight formation problem, in horizontal plane, of multiple unmanned aerial vehicles (UAVs) kind quadrotor, by means of a leader-follower scheme. By Topic Aerospace Bioengineering Communication, Networking & Broadcasting Components, Circuits, Devices & Systems Computing & Processing Engineered Materials, Dielectrics & Plasmas Engineering Profession Fields, Waves & Electromagnetics General Topics for Engineers Geoscience Nuclear Engineering Photonics & Electro-Optics Power, Energy, & Industry Applications Robotics & Control Systems Signal Processing & Analysis Transportation . A sliding mode controller is proposed for the translational dynamic and provides the desired orientation for the UAV, which is controlled by a linear PD control. Learn more about: IEEE membership IEEE Xplore subscriptions Item has been added to the cart. Please enable JavaScript to use all the features on this page. The paper presents experimental results validating the performance of the formation control laws using a ‘virtual leader’ configuration.KeywordsFormation flight; Guidance; UAV; Non-linear control; Non-linear dynamic inversion; Feedback linearizationCorresponding author. The first phase of flight tests was performed with the goal of exciting all the aircraft dynamic modes. Click the View full text link to bypass dynamically loaded article content. The recorded flight data were then used for a parameter identification study. Mercado ;Dept.

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