Comparison of Fixed and Variable Pitch Actuators for Agile Quadrotors

Comparison of Fixed and Variable Pitch Actuators for Agile Quadrotors

This paper presents the design, analysis and experimental testing of a variable- pitch quadrotor. A custom in-lab built quadrotor with on-board attitude stabi- lization is developed and tested. An analysis of the dynamic di erences in thrust output between a xed-pitch and variable-pitch propeller is...

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Bibliographic Details
Main Authors: Cutler, Mark Johnson (Contributor), Ure, Nazim Kemal (Contributor), Michini, Bernard J. (Contributor), How, Jonathan P. (Contributor)
Other Authors: Massachusetts Institute of Technology. Aerospace Controls Laboratory (Contributor), Massachusetts Institute of Technology. Department of Aeronautics and Astronautics (Contributor)
Format: Article
Language:English
Published: American Institute of Aeromautics and Astronautics, 2013-11-07T20:16:08Z.
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