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Performance Modeling of Urban Air Mobility Vehicles to Support Air Traffic Management ResearchThe recent emergence of Urban Air Mobility (UAM) vehicles has resulted in a need for flight performance models that enable comprehensive simulation-based research on air traffic management topics such as route structure, scheduling, and separation standards. Successful performance modeling methods exist for a wide range of traditional aircraft designs. However, comparable modeling methods appropriate for UAM vehicles that combine fixed-wing and rotorcraft performance have not yet been established. One challenge to progress has been the lack of available data capturing the performance characteristics and unique flight profiles of these aircraft. This paper describes methods used to generate the required performance data and the development of performance models for UAM vehicles. Included is a review of the energy and power equations often used in developing performance models for traditional aircraft as well as a discussion of their applicability to UAM vehicles. The challenge of generating realistic performance data in over-actuated vehicles transitioning from hover to cruise flight is also addressed through an approach based on objective function optimization. A table-based performance model format adapted to UAM configurations is described, as well as parametric models intended to accompany the performance table to allow detailed modeling of power and fuel consumption during accelerated flight, turning flight, or flight at an arbitrary climb or descent rate. A discussion of future work is also provided, including the need for refinement of UAM performance modeling methods and formats, especially in conjunction with improvements to aerodynamic modeling of vehicles with complex designs where strong interaction effects may dominate important regions of the flight envelope.
Document ID
20220017406
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
David Hartman
(Langley Research Center Hampton, Virginia, United States)
John Foster
(Langley Research Center Hampton, Virginia, United States)
Christopher Hartman
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
November 18, 2022
Publication Date
January 19, 2023
Publication Information
Publication: AIAA SCITECH 2023 Forum
Publisher: American Institute of Aeronautics and Astronautics
e-ISBN: 9781624106996
Subject Category
Air Transportation and Safety
Report/Patent Number
AIAA-2023-0548
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: National Harbor, MD
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80LARC17C0003
WBS: 629660.04.31.07.10
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Base of Aircraft Data
Calibrated Airspeed
Aircraft Design
Aircraft Operations
Fuel Consumption
Aircraft Performance
Flight Envelope
Rotary Wing
Trajectory Prediction
Air Traffic Management (ATM)
Urban Air Mobility (UAM)
ATM-X
Performance Modeling
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