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Differential amplitude angle guidance

阅读:460发布:2021-03-16

专利汇可以提供Differential amplitude angle guidance专利检索,专利查询,专利分析的服务。并且An instrument landing system is operable with a scanning beam antenna system for providing glideslope and runway centerline indications to an aircraft. An azimuth antenna rotates in a plane parallel to the earth''s surface. An elevation antenna rotates in a plane normal to the earth''s surface. A first pair of AM modulated tones represents the instantaneous position of the azimuth antenna and a second pair of AM modulated tones represents the instantaneous position of the elevation antenna. A first carrier signal is modulated with the first pair of tones and a second carrier signal is modulated with the second pair of tones. The first and second carrier signals are received in the aircraft and when the first and second carrier signals illuminate the position in space occupied by the aircraft, the two pairs of tones are detected and their relative amplitudes are compared, wherein equal amplitudes indicate proper glideslope and/or centerline of runway.,下面是Differential amplitude angle guidance专利的具体信息内容。

1. An instrument landing system operable with a scanning beam antenna system for providing glideslope and runway centerline indications to an aircraft comprising: a. an azimuth antenna rotating in a plane parallel to the earth''s surface; b. an elevation antenna rotating in a plane normal to the earth''s surface; c. first means for generating a first pair of AM modulated tones representing the instantaneous position of said aximuth antenna, said tones having substantially equal amplitudes when the antenna is aligned with the runway; d. second means for generating a second pair of AM modulated tones representing the instantaneous position of said elevation antenna, said tones having substantially equal amplitudes when the antenna is aligned with the correct glideslope; e. azimuth transmitter means coupled to the azimuth antenna for generating a first carrier signal having a predetermined frequency, and elevation transmitter means coupled to the elevation antenna for generating a second carrier signal having a second predetermined frequency; f. means for FM modulating said first carrier signal with said first pair of tones and said second carrier signal with said second pair of tones; g. airborne means for receiving said first and second carrier signals; h. means for detecting when said first and second carrier signals are illuminating the position in space occupied by said aircraft; and i. means for detecting said two pairs of tones ane comparing their relative amplitude, wherein equal amplitudes indicate proper glideslope and/or centerline of runway.
2. The instrument landing system claimed in claim 1 wherein said FM modulating means includes baseband modulators.
3. The instrument landing system claimed in claim 2 including azimuth angle encoding means for encoding the instantaneous position of said azimuth antenna and inputting said position to said first generating means, and elevation angle encoding means for encoding the instantaneous position of said elevation antenna and inputting said position to said second generating means.
4. The instrument landing system claimed in claim 3 including means for indicating the relative glideslope of said runway.
5. The instrument landing system claimed in claim 4 where said first and second generating means are crystal oscillators generating pulses at predetermined rates and read only memories, said read only memories containing predetermined waveform values addressed by said crystal oscillators to provide said tone signals.
6. The instrument landing system claimed in claim 5 wherein said detecting and comparing means include means for separating each pair of tones into their separate channels, and means for indicating the erroR between said pairs of tones.
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