DocumentCode :
1125375
Title :
An Aircraft Noise Pollution Model for Tra jectory Optimization
Author :
Atalay Barkana ; Dmma ; Gerald Cook
Author_Institution :
Eskis¿ehir, Turkey
Issue :
2
fYear :
1976
fDate :
3/1/1976 12:00:00 AM
Firstpage :
109
Lastpage :
116
Abstract :
The mobility of our society makes effective and efficient operation of our air terminals a necessity. For this reason, landing trajectories must be optimized. One important factor in the performance index is aircraft noise received by people residing near the terminal. This paper develops a mathematical model of this noise effect so that it may be included in the performance index. The model yields the boundary on the ground inside of which the noise level is at or above 70 dB. This area can be weighted with the population density. The model compares very favorably with available data.
Keywords :
Aerospace electronics; Aircraft; Geometry; Mathematical model; NASA; Noise level; Noise measurement; Performance analysis; Pollution; Transportation;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1976.308274
Filename :
4101609
Link To Document :
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