Flight Trajectory Optimization to Minimize Ground Noise in Helicopter Landing Approach
Author:
Affiliation:
1. University of Tokyo, Tokyo 113-8656, Japan
2. Japan Aerospace Exploration Agency, Tokyo 182-8522, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34458
Reference13 articles.
1. Noise-Minimum Runway-Independent Aircraft Approach Design for Baltimore-Washington International Airport
2. Toward Noise Abatement Flight Procedure Design: DLR Rotorcraft Noise Ground Footprints Model
3. Optimization of Flexible Approach Trajectories Using a Genetic Algorithm
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