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Dynamic Replanning of Low Noise Rotorcraft OperationsA new method for rapidly planning and dynamically replanning low noise rotorcraft flight operations is developed. A large database of rotorcraft maneuver segments is generated, and an acoustic cost is assigned to each segment by using a computationally efficient semiempirical rotorcraft noise modeling method that accurately models the changes in rotor noise caused by maneuvering flight. Combinatoric optimization techniques are then employed to combine these maneuver segments into a low noise optimal flight path. A simple heuristic for estimating the total acoustic cost required to reach the target location is developed and incorporated into the search algorithm, allowing the computation of low noise paths in seconds. A procedure for implementing an “anytime” version of the method is described, enabling feasible solutions to be dynamically replanned “on the fly”—i.e., in fractions of a second—and refined over time to a low noise optimal solution.






Document ID
20200002612
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Greenwood, Eric
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 17, 2020
Publication Date
May 13, 2019
Subject Category
Acoustics
Report/Patent Number
NF1676L-31490
Report Number: NF1676L-31490
Meeting Information
Meeting: Vertical Flight Society Annual Forum and Technology Display
Location: Philadelphia, PA
Country: United States
Start Date: May 13, 2019
End Date: May 16, 2019
Sponsors: Vertical Flight Society
Funding Number(s)
WBS: 664817.02.07.03.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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