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A Model Predictive Control Approach for In-Flight Acoustic Constraint ComplianceVehicle noise remains one of the major barriers to public acceptance of Urban Air Mobility-class aircraft. This work focuses on motion planning for aircraft in noise-sensitive areas. A nonlinear Model Predictive Path Integral (MPPI) control law is used to generate a finite-horizon trajectory that satisfies acoustic level constraints at a set of (three-dimensional) observer locations. The MPPI framework places no restrictions on the class of state-dependent cost functionals that can be employed, making it well-suited for use with sophisticated acoustic models and metrics, in addition to dynamic and mission-relevant constraints. The model predictive control architecture is also suitable for implementation in a real-time application. A simulation example demonstrates the ability of the controller to modify the flight trajectory in order to satisfy acoustic constraints at multiple measurement locations.
Document ID
20205011352
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Kasey A Ackerman
(Langley Research Center Hampton, Virginia, United States)
Irene M Gregory
(Langley Research Center Hampton, Virginia, United States)
Evangelos A Theodorou
(Georgia Institute of Technology Atlanta, Georgia, United States)
Naira Hovakimyan
(University of Illinois at Urbana Champaign Urbana, Illinois, United States)
Date Acquired
December 9, 2020
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA-2021-1958
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
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: 664817.02.07.03.02.04
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
Keywords
acoustically-aware vehicle
UAM
Model Predictive Control
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