Title:
計器着陸システム(ILS)のための滑空経路送信装置
Document Type and Number:
Japanese Patent JP4112635
Kind Code:
B2
Abstract:
PCT No. PCT/EP98/03661 Sec. 371 Date Mar. 24, 1999 Sec. 102(e) Date Mar. 24, 1999 PCT Filed May 22, 1998 PCT Pub. No. WO98/54546 PCT Pub. Date Dec. 3, 1998A glide path transmitter for an instrument landing system. The transmitter includes several antenna radiators by way of which high frequency signals containing various low frequency modulated carrier and side band components are radiated. The components overlap each other in the far field where they form a guide signal which can be evaluated by aircraft. Phases of the carrier oscillations of the radiated high frequency signals form the guide signal having a set relationship with each other. A separate digitally controlled modulator is provided for each high frequency signal fed to an antenna radiator. The modulator modulates the phase and amplitude of a high frequency oscillation fed thereto according to a given model and inputs the modulated high frequency signal into the antenna radiator allocated thereto, thus reducing the supply network expenditure.
Inventors:
Ruprecht, liner
Stammelbach, Jurgen
Kleiber, Herbert
Stammelbach, Jurgen
Kleiber, Herbert
Application Number:
JP50027299A
Publication Date:
July 02, 2008
Filing Date:
May 22, 1998
Export Citation:
Assignee:
Airsys Navigation Systems Game Behr
International Classes:
G01S1/14; G01D1/06; G01S1/18; G08G5/02
Domestic Patent References:
| JP5281336A | ||||
| JP7333312A | ||||
| JP3220804A | ||||
| JP3145303A | ||||
| JP4290969A | ||||
| JP8005725A |
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori
Kobayashi Yoshinori