DocumentCode :
1688615
Title :
Hybrid model to evaluate the aircraft landing environment
Author :
Wu, Huaxin ; Zhao, Xiubin ; Dai, Chuanjin
Author_Institution :
Telecommun. Eng. Inst., Air Force Eng. Univ., Xi´´an, China
fYear :
2010
Firstpage :
5929
Lastpage :
5932
Abstract :
Aircraft landing environment has much influence on approach landing systems and it is a preferred way to perform a system simulation and prediction for system performance in the scattering environment to ensure security instead of performing flight inspection. Hybrid evaluation system for aircraft landing environment is firstly outlined, and then the hybrid model to simulate the systems considering the effect of environment is proposed and discussed. Multi-scattering effect is included in the model. Practical application example using the model to evaluate aircraft landing environment is presented, and results show the effectiveness of the hybrid evaluation system.
Keywords :
aircraft landing guidance; electromagnetic wave scattering; aircraft landing systems; flight inspection; hybrid evaluation system; hybrid model; multi-scattering effect; Aircraft; Aircraft manufacture; Airports; Analytical models; Atmospheric modeling; Buildings; Scattering; Approach Landing System; Multipath Effect; System Evaluation; System Modeling;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Automation (WCICA), 2010 8th World Congress on
Conference_Location :
Jinan
Print_ISBN :
978-1-4244-6712-9
Type :
conf
DOI :
10.1109/WCICA.2010.5554489
Filename :
5554489
Link To Document :
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