System is proposed for landing aircraft under zero-visibility and high-turbulence atmospheric conditions, which is primarily airborne, except for possible use of ground-based radar beacons, and is constructed with light, inexpensive, and reliable components.
Longitudinal guidance system for aircraft landing during flare-out
Automatic Remote Control -- Proc
2nd Congress of International Federation of Automatic Control ; 1964 Landing
1964
8 pages
Conference paper
English
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The landing flare of large transport aircraft
TIBKAT | 1969
|The Landing Flare of Large Transport Aircraft
NTIS | 1967
|European Patent Office | 2021
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