Hybrid Electromagnetic Simulation Using 2D-FDTD and Ray-Tracing Methods for Airport Surfaces-Reference-Cited by-同舟云学术

Hybrid Electromagnetic Simulation Using 2D-FDTD and Ray-Tracing Methods for Airport Surfaces

Published:2023-11-01 Issue:11 Volume:E106.C Page:774-779
ISSN:0916-8524
Container-title:IEICE Transactions on Electronics
language:en
Short-container-title:IEICE Trans. Electron.

Author:

SUGA Ryosuke¹,WATANABE Megumi¹,KEZUKA Atsushi²

Affiliation:

1. Department of Eletrical Engineering and Electronics, Aoyama Gakuin University

2. Electrical Navigation Research Institute, National Institute of Maritime, Port and Aviation Technology

Publisher

Institute of Electronics, Information and Communications Engineers (IEICE)

Subject

Electrical and Electronic Engineering,Electronic, Optical and Magnetic Materials

Link

https://www.jstage.jst.go.jp/article/transele/E106.C/11/E106.C_2022ECP5068/_pdf

Reference32 articles.

1. [1] R. Sabatini, T. Moore, and C. Hill, “A novel GNSS integrity augmentation system for civil and military aircraft,” Int. J. Mech. Aerosp. Ind. Mech. Eng, vol.7, no.12, pp.1433-1449, Dec. 2013.

2. [2] S. Saitoh, S. Fukushima, T. Yoshihara, and N. Fujii, “Experimental GBAS performance at the approach phase,” Proc. ION 2003 Nat. Tech. Meeting, pp.317-325, Jan. 2003.

3. [3] L. Andreas, A. Quiles, M. Reche, W. Dunkel, and S. Grand-Perret, “Initial GBAS experiences in Europe,” Proc. 18th Int. Tech. Meeting of the Satellite Division of the Inst. Navig., vol.2005, pp.2911-2922, Sept. 2005.

4. [4] C. Kee, S. Park, and Y. Yun, “Comparative study between GBAS and conventional aircraft precision approach guidance system,” Trans. Japan Soc. Aeronaut. Space Sci., vol.46, no.154, pp.224-229, Feb. 2004. 10.2322/tjsass.46.224

5. [5] M. Felux, T. Dautermann, and H. Becker, “GBAS landing system-precision approach guidance after ILS,” Aircraft Eng. Aerosp. Tech., vol.85, no.5, pp.382-388, Aug. 2013. 10.1108/aeat-07-2012-0115