NASA NTRS · 20205002913
A Model Predictive Control Approach for In-Flight Acoustic Constraint Compliance
Abstract
Vehicle 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 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 proposed control law 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.
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Kasey A. Ackerman, Irene M. Gregory. A Model Predictive Control Approach for In-Flight Acoustic Constraint Compliance. https://ntrs.nasa.gov/citations/20205002913
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