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Revolutionary Vertical Lift Technology Lift + Cruise Concept Vehicle Powertrain Dynamic ModelThe Lift + Cruise (L+C) is one of several Revolutionary Vertical Lift Technology (RVLT) concept aircraft identified by NASA to investigate Urban Air Mobility (UAM) requirements. This six-passenger vehicle has a conventional tube-and-wing configuration, but with eight lift rotors (four on each wing) and a pusher rotor on the tail. This arrangement allows it to take off and land vertically as well as fly like an airplane. This report presents a novel dynamic model of the L+C powertrain built using the Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS) and the Electrical Modeling and Thermal Analysis Toolbox (EMTAT), both of which are NASA-developed toolboxes, and together are capable of modeling hybrid-electric powertrain architectures. This research effort models the complex behavior of the powertrain at the mechanical timescale (15 to 20 ms). The model consists of a turboshaft engine, generator, direct current bus, energy storage management system, gearboxes, and electric propulsor systems coupled together to create a dynamic model that mimics the operation of the multidomain powertrain. Two control algorithms, designed to equalize the power consumed to the power produced, are compared to assess their practicality: (1) independent proportional-integral (PI) control and (2) linear quadratic integral regulator (LQIR) control. Simulation results highlight the key features present in the model and demonstrate its operation under the two control schemes.
Document ID
20230018312
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Santino J. Bianco
(Glenn Research Center Cleveland, United States)
Jonathan S. Litt
(Glenn Research Center Cleveland, United States)
Jeffryes W. Chapman
(Glenn Research Center Cleveland, United States)
Jonah J. Sachs-Wetstone
(Case Western Reserve University Cleveland, Ohio, United States)
Edgar Garcia Duran
(National Space Grant Foundation Washington D.C., District of Columbia, United States)
Parker Dentino
(The University of Texas at Austin Austin, United States)
Date Acquired
December 18, 2023
Publication Date
February 1, 2024
Subject Category
Aircraft Propulsion and Power
Funding Number(s)
WBS: 109492.02.03.06.05.02
CONTRACT_GRANT: 80NSSC19M0235
CONTRACT_GRANT: 80GRC019D0001
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Technical Management
Keywords
revolutionary vertical lift technology
lift+cruise
concept
powertrain
dynamic
model
electrified
aircraft
propulsion
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