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Power Optimal Control Allocation for Distributed Electric Propulsion in a Series/Parallel Hybrid PowertrainThis paper describes a thrust allocation scheme that minimizes power consumption in an electrified powertrain with Distributed Electric Propulsion. It takes advantage of an observation about component efficiency maps, that efficiency is often highest at high torque/high speed conditions. This optimal approach is demonstrated to satisfy total thrust and net yaw axis torque requirements, making it suitable for utilizing differential thrust for maneuvering.
Document ID
20260004797
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Jonathan S Litt
(Glenn Research Center Cleveland, United States)
Date Acquired
May 27, 2026
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
AIAA-2026-4687
Meeting Information
Meeting: AIAA Aviation Forum
Location: San Diego, CA
Country: US
Start Date: June 8, 2026
End Date: June 12, 2026
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 361807.02.03.03.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
electrified aircraft propulsion
Electrified powertrain
optimal control
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