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Examination of Unified Control Approaches Incorporating Generalized Control AllocationTransition vehicles which combine vertical take off and landing with cruise configurations pose a unique challenge for control design and implementation. For this class of vehicle, successful control designs have historically broken the flight envelope into phases and modified the control approach for each phase. This research approaches control in a unified way across the entire envelope using a robust optimal design which provides effector weighting then implemented in a generalized Affine Generalized Inverse control allocation algorithm. System performance for a Lift plus Cruise transition vehicle is presented.
Document ID
20205010869
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Michael J. Acheson
(Langley Research Center Hampton, Virginia, United States)
Jacob Cook
(Langley Research Center Hampton, Virginia, United States)
Irene Gregory
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
December 1, 2020
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: AIAA SciTech Forum and Exposition 2021
Location: Virtual
Country: US
Start Date: January 11, 2021
End Date: January 21, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109492.02.07.07.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
unified control, robust control, optimal control, transition vehicles, control allocation
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