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System Identification for a Subscale Tiltrotor eVTOL Aircraft from Hover Flight-Test Data
Document ID
20260000047
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Benjamin M Simmons
(Langley Research Center Hampton, United States)
Kasey A Ackerman
(Langley Research Center Hampton, United States)
Date Acquired
January 5, 2026
Subject Category
Aircraft Stability and Control
Aircraft Design, Testing and Performance
Meeting Information
Meeting: AIAA SciTech Forum 2026
Location: Orlando, FL
Country: US
Start Date: January 12, 2026
End Date: January 16, 2026
Sponsors: American Institute of Aeronautics and Astronautics - AIAA
Funding Number(s)
WBS: 361807.02.07.05.01
WBS: 107210.02.21.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
RAVEN
UAM
AAM
eVTOL
multisine inputs
distributed electric propulsion
vertical takeoff and landing
flight test
aero-propulsive modeling
system identification