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Landing approach guidance system for aircraft using electronic radio navigation system specifying electronic guide path with predetermined glide path angle
Landing approach guidance system for aircraft using electronic radio navigation system specifying electronic guide path with predetermined glide path angle
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机译：使用电子无线电导航系统的飞机着陆进近制导系统，该系统指定具有预定滑行角的电子导引路径
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摘要
The landing approach guidance system (1) enables successive approach of several aircraft. A first aircraft assigned along one of the landing paths, is guided on a first electronic guide path with a first glide path angle to a first touch down threshold on the landing path. The second following aircraft is guided along a higher second electronic guide path with a second glide path angle to a second touch down threshold on the landing path. The higher glide path compared to the first glide path is guided at a steeper angle. For the radio navigation with the landing approach of the first aircraft of the first electronic path and for the radio navigation with the landing approach of the following second aircraft, the top second electronic guide path is selected.
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