US PATENT SUBCLASS 244 / 187
.~.~.~.~.~ With "flare-out" detection

Current as of: June, 1999
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244 /   HD   AERONAUTICS

75 R  DF  AIRCRAFT CONTROL {8}
76 R  DF  .~ Automatic {10}
175  DF  .~.~ Electric course control {10}
183  DF  .~.~.~ Of aircraft on its landing course {2}
186  DF  .~.~.~.~ Vertical glide path control {2}
187.~.~.~.~.~ With "flare-out" detection

DEFINITION

Classification: 244/187

(under subclass 186) System wherein the direction of the aircraft during landing is changed from a first path to a second path, the first path being inclined to the ground and the second path being parallel to and close to the ground, the change being responsive to a sensing of the altitude of the aircraft to cause a change of inclination of the aircraft.