The purpose of this work was to create a six degree of freedom balance that could produce meaningful data for micro aerial vehicles. Research was conducted to investigate the common balance configurations, and the strengths and weaknesses of each configuration were used to select the most appropriate design. The limitations of available fabrication facilities, the desired level of performance and the end user of the balance were all considered to finalize the design. The balance and data acquisition system were fabricated over a period of several months, and unforeseen design issues were handled forthwith. Rigorous calibration and testing processes were conducted. The results of the calibration and testing processes were analyzed and documented. The performance of the balance was determined to be less than traditionally recommended, but was acceptable due to the small magnitude of the loads. Further testing is recommended to determine if performance improves as the balance settles.
","abstract_html":"<p>The purpose of this work was to create a six degree of freedom balance that could produce meaningful data for micro aerial vehicles. Research was conducted to investigate the common balance configurations, and the strengths and weaknesses of each configuration were used to select the most appropriate design. The limitations of available fabrication facilities, the desired level of performance and the end user of the balance were all considered to finalize the design. The balance and data acquisition system were fabricated over a period of several months, and unforeseen design issues were handled forthwith. Rigorous calibration and testing processes were conducted. The results of the calibration and testing processes were analyzed and documented. The performance of the balance was determined to be less than traditionally recommended, but was acceptable due to the small magnitude of the loads. Further testing is recommended to determine if performance improves as the balance settles.</p>","abstract_has_math":false,"creators":["King, Michael Christopher"],"institution":null,"degree_name":"Master of Science in Aerospace Engineering","degree_level":"Thesis - Open Access","degree_discipline":"Aerospace Engineering","degree_department":null,"school":null,"contributors":[],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2012,"date_issued":"2012-04-01T07:00:00Z","date_published":"2012-04-01T07:00:00Z","updated_at":"2026-07-27T19:26:02Z","subjects":["micro vehicles","aerial vehicles","Aeronautical Vehicles","Aerospace Engineering"],"languages":[],"rights":[],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"https://commons.erau.edu/edt/89","outbound_label":"Repository record","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:creator","label":"Author","values":["King, Michael Christopher"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"thesis:degree_discipline","label":"Discipline","values":["Aerospace Engineering"]},{"key":"thesis:degree_level","label":"Degree Level","values":["Thesis - Open Access"]},{"key":"thesis:degree_name","label":"Degree Name","values":["Master of Science in Aerospace Engineering"]}]},{"id":"subjects_keywords","label":"Subjects and Keywords","entries":[{"key":"dc:subject","label":"Dc Subject","values":["micro vehicles","aerial vehicles","Aeronautical Vehicles","Aerospace Engineering"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["https://commons.erau.edu/edt/89"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description.abstract","label":"Abstract","values":["The purpose of this work was to create a six degree of freedom balance that could produce meaningful data for micro aerial vehicles. Research was conducted to investigate the common balance configurations, and the strengths and weaknesses of each configuration were used to select the most appropriate design. The limitations of available fabrication facilities, the desired level of performance and the end user of the balance were all considered to finalize the design. The balance and data acquisition system were fabricated over a period of several months, and unforeseen design issues were handled forthwith. Rigorous calibration and testing processes were conducted. The results of the calibration and testing processes were analyzed and documented. The performance of the balance was determined to be less than traditionally recommended, but was acceptable due to the small magnitude of the loads. Further testing is recommended to determine if performance improves as the balance settles.
"]},{"key":"dc:title","label":"Title","values":["The Development of a Force Balance for Testing Micro Aerial Vehicles"]}]}],"canonical_facts":{"dc:creator":["King, Michael Christopher"],"dc:description.abstract":["The purpose of this work was to create a six degree of freedom balance that could produce meaningful data for micro aerial vehicles. Research was conducted to investigate the common balance configurations, and the strengths and weaknesses of each configuration were used to select the most appropriate design. The limitations of available fabrication facilities, the desired level of performance and the end user of the balance were all considered to finalize the design. The balance and data acquisition system were fabricated over a period of several months, and unforeseen design issues were handled forthwith. Rigorous calibration and testing processes were conducted. The results of the calibration and testing processes were analyzed and documented. The performance of the balance was determined to be less than traditionally recommended, but was acceptable due to the small magnitude of the loads. Further testing is recommended to determine if performance improves as the balance settles.
"],"dc:identifier":["https://commons.erau.edu/edt/89"],"dc:subject":["micro vehicles","aerial vehicles","Aeronautical Vehicles","Aerospace Engineering"],"dc:title":["The Development of a Force Balance for Testing Micro Aerial Vehicles"],"thesis:degree_discipline":["Aerospace Engineering"],"thesis:degree_level":["Thesis - Open Access"],"thesis:degree_name":["Master of Science in Aerospace Engineering"]},"updated_at":"2026-07-27T19:26:02Z"}