電子航法研究所報告
Online ISSN : 2758-2973
Print ISSN : 1341-9102
TRSB方式MLS方位誘導システムの試作と測角実験
松本 千秋片野 忠夫朝倉 道弘
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研究報告書・技術報告書 フリー

1978 年 1978 巻 22 号 p. 1-22

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The microwave landing system (MLS) is under development as a replacement for the VHF/UHF ILS. The time refference scanning beam system (TRSB) was selected as the preferred system for worldwide standardization by ICAO AWO Divisional Meeting recently.

This paper discribes experimental model of TRSB-MLS azimuth subsystem and experimental study of angle guidance error.

The azimuth subsystem consists of azimuth guidance antenna which includes a sector omni antenna and a scanning beam antenna, transmitter, and airborne receiver. The scanning beam antenna is linear phased array. This antenna has a 3 degrees azimuth beam width which is electronically scanned ±40 degrees in azimuth, and has a 0 to 20 degrees elevation coverage with a sharp underside cutoff for multipath reduction.

The transmitter employs TWT for the final stage of amplification, and radiates 10 watts of CW power at 5 GHz.

Effectiveness of reduction of angle guidance error by smoothing of received signal, and error due to threshold level variation in the receiver envelope processor are examined with the experiments using the azimuth subsystem. Experimental results show that the error can be reduced by decreasing the bandwidth of envelope processing circuit, and accuracy of 0.04 degrees is obtained over azimuth coverage.

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© 1978 国立研究開発法人 海上・港湾・航空技術研究所電子航法研究所
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