Abstract
A new method for rapidly planning and dynamically replanning low noise rotorcraft flight operations has been developed and is discussed. 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.
Original language | English (US) |
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State | Published - Jan 1 2019 |
Event | Vertical Flight Society's 75th Annual Forum and Technology Display - Philadelphia, United States Duration: May 13 2019 → May 16 2019 |
Conference
Conference | Vertical Flight Society's 75th Annual Forum and Technology Display |
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Country/Territory | United States |
City | Philadelphia |
Period | 5/13/19 → 5/16/19 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Control and Systems Engineering