Design of Quiet Rotorcraft Approach Trajectories

By: Nasa, National Aeronautics and Space Adm

A optimization procedure for identifying quiet rotorcraft approach trajectories is proposed and demonstrated. The procedure employs a multi-objective genetic algorithm in order to reduce noise and create approach paths that will be acceptable to pilots and passengers. The concept is demonstrated by application to two different helicopters. The optimized paths are compared with one another and to a standard 6-deg approach path. The two demonstration cases validate the optimization procedure but highlight the need for improved noise prediction techniques and for additional rotorcraft acoustic data sets. Padula, Sharon L. and Burley, Casey L. and Boyd, D. Douglas, Jr. and Marcolini, Michael A. Langley Research Center WBS 877868.02.07.07

• Format: Paperback
• Language: English
• ISBN: 179391544X
• ISBN13: 9781793915443
• Release Date: January 1
• Publisher: Independently Published
• Length: 32 Pages
• Weight: 0.22 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"