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Inexpensive Multirotor Platform for Advanced Controls Testing (IMPACT): Development, Integration, and ExperimentationA comprehensive framework was explored and validated for rapid deployment and testing of custom flight control logic using the Inexpensive Multirotor Platform for Advanced Controls Testing (IMPACT). This vehicle facilitated the efficient validation and refinement of a custom flight control algorithm, which was designed using Simulink and deployed onto a Pixhawk flight computer running PX4 firmware through the utilization of the MathWorks UAV Toolbox. The robust and cost-effective design of IMPACT provides the groundwork for future flight testing of flight controls and model development research for electric vertical takeoff and landing (eVTOL) aircraft.
Document ID
20240000223
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Garrett D Asper
(Langley Research Center Hampton, United States)
Benjamin M Simmons
(Langley Research Center Hampton, United States)
Rachel M Axten
(Langley Research Center Hampton, United States)
Kasey A Ackerman
(Langley Research Center Hampton, United States)
Patrick E Corrigan
(Office of STEM Engagement (OSTEM) Internship Program)
Date Acquired
January 6, 2024
Publication Date
March 1, 2024
Subject Category
Aircraft Design, Testing and Performance
Aircraft Stability and Control
Report/Patent Number
NASA/TM-20240000223
Funding Number(s)
WBS: 109492.02.07.07.05
WBS: 109492.02.07.07.07
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
flight testing
flight controls
system identification
PX4
Pixhawk
UAV
IMPACT
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