{"id":{"repo_id":"uiuc","oai_identifier":"oai:www.ideals.illinois.edu:2142/106288"},"canonical_url":"https://search.dev.ndltd.org/etd/uiuc/oai:www.ideals.illinois.edu:2142/106288","repository":{"repo_id":"uiuc","name":"University of Illinois - Urbana-Champaign","base_url":"https://www.ideals.illinois.edu/oai-pmh"},"display":{"title":"A model of quadrotor UAV power consumption and its performance across a range of flight conditions","abstract":"This thesis presents a parametric model of quadrotor power consumption and characterizes the performance of this model in hardware experiments. Like other existing power models that have been used both for quadrotors and general rotorcraft, it can be expressed as the sum of four terms---induced, parasitic, profile, and climb power---that depend on estimates of the aerodynamic forces and moments acting on the quadrotor. The model's accuracy was measured across a wide range of flight conditions. The results of an ablation study to show the relative contribution of each term are presented, concluding that the contribution strongly depends on the ground velocity of the quadrotor. Both the dataset and code are freely available as a benchmark to facilitate future work in this area.","abstract_html":"This thesis presents a parametric model of quadrotor power consumption and characterizes the performance of this model in hardware experiments. Like other existing power models that have been used both for quadrotors and general rotorcraft, it can be expressed as the sum of four terms---induced, parasitic, profile, and climb power---that depend on estimates of the aerodynamic forces and moments acting on the quadrotor. The model's accuracy was measured across a wide range of flight conditions. The results of an ablation study to show the relative contribution of each term are presented, concluding that the contribution strongly depends on the ground velocity of the quadrotor. Both the dataset and code are freely available as a benchmark to facilitate future work in this area.","abstract_has_math":false,"creators":["Faustino, Alexander B."],"institution":"University of Illinois at Urbana-Champaign","degree_name":"M.S.","degree_level":"Thesis","degree_discipline":"Aerospace Engineering","degree_department":null,"school":null,"contributors":["Bretl, Timothy"],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2020,"date_issued":"2020-03-02T22:03:27Z","date_published":"2020-03-02T22:03:27Z","updated_at":"2026-07-22T22:24:45Z","subjects":["Quadrotor UAVs","UAV power modeling"],"languages":["en"],"rights":["Copyright 2019 Alexander Faustino"],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"http://hdl.handle.net/2142/106288","outbound_label":"Handle","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor","label":"Contributor","values":["Bretl, Timothy"]},{"key":"dc:creator","label":"Author","values":["Faustino, Alexander B."]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date","label":"Dc Date","values":["2020-03-02T22:03:27Z","2019-12-12","2019-12"]},{"key":"dc:type","label":"Dc Type","values":["text"]},{"key":"thesis:degree_discipline","label":"Discipline","values":["Aerospace Engineering"]},{"key":"thesis:degree_level","label":"Degree Level","values":["Thesis"]},{"key":"thesis:degree_name","label":"Degree Name","values":["M.S."]},{"key":"thesis:institution_name","label":"Thesis Institution Name","values":["University of Illinois at Urbana-Champaign"]}]},{"id":"subjects_keywords","label":"Subjects and Keywords","entries":[{"key":"dc:subject","label":"Dc Subject","values":["Quadrotor UAVs","UAV power modeling"]}]},{"id":"language_rights","label":"Language and Rights","entries":[{"key":"dc:language","label":"Dc Language","values":["en"]},{"key":"dc:rights","label":"Dc Rights","values":["Copyright 2019 Alexander Faustino"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["http://hdl.handle.net/2142/106288"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description","label":"Description","values":["This thesis presents a parametric model of quadrotor power consumption and characterizes the performance of this model in hardware experiments. Like other existing power models that have been used both for quadrotors and general rotorcraft, it can be expressed as the sum of four terms---induced, parasitic, profile, and climb power---that depend on estimates of the aerodynamic forces and moments acting on the quadrotor. The model's accuracy was measured across a wide range of flight conditions. The results of an ablation study to show the relative contribution of each term are presented, concluding that the contribution strongly depends on the ground velocity of the quadrotor. Both the dataset and code are freely available as a benchmark to facilitate future work in this area.","Submission original under an indefinite embargo labeled 'Open Access'. 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Like other existing power models that have been used both for quadrotors and general rotorcraft, it can be expressed as the sum of four terms---induced, parasitic, profile, and climb power---that depend on estimates of the aerodynamic forces and moments acting on the quadrotor. The model's accuracy was measured across a wide range of flight conditions. The results of an ablation study to show the relative contribution of each term are presented, concluding that the contribution strongly depends on the ground velocity of the quadrotor. Both the dataset and code are freely available as a benchmark to facilitate future work in this area.","Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2020-02-28 without embargo terms","The student, Alexander Faustino, accepted the attached license on 2019-12-11 at 17:02.","The student, Alexander Faustino, submitted this Thesis for approval on 2019-12-11 at 17:09.","This Thesis was approved for publication on 2019-12-12 at 08:28.","DSpace SAF Submission Ingestion Package generated from Vireo submission #14805 on 2020-02-28 at 17:16:49","Made available in DSpace on 2020-03-02T22:03:27Z (GMT). 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