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MICRO AIRCRAFT DESIGN DBF-2017

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The goal of this MQP was to design, build, and fly a UAV that can successfully complete the four missions of the AIAA DBF 2017 competition while optimizing the team’s score and meeting the general competition requirements. The UAV was an electric-driven, radio controlled aircraft that must be powered by nickel batteries, and fit inside a fixed-dimension, watertight launch tube in a folded storage configuration. The UAV must be capable of unfolding from the storage configuration to the flight configuration without the use of any tools, all moveable components be self-locking and self-aligning. The UAV must complete three flight missions that evaluate aircraft speed and the ability to carry a payload and one ground mission.

  • This report represents the work of one or more WPI undergraduate students submitted to the faculty as evidence of completion of a degree requirement. WPI routinely publishes these reports on its website without editorial or peer review.
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  • E-project-042617-180757
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  • 2017
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Date created
  • 2017-04-26
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