US PATENT SUBCLASS 244 / 184
.~.~.~.~ By steering or yaw

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}
184.~.~.~.~ By steering or yaw {1}
185  DF  .~.~.~.~.~> And vertical glide path control

DEFINITION

Classification: 244/184

(under subclass 183) System wherein the direction of the aircraft, or its orientation relative to its glide path, is changed from right to left or vice versa, the change occurring in an inclined plane; the inclined plane being one wherein two lines intersect, one of the lines being a horizontal line and the other line being said inclined glide path line of subclass 183.

(1) Note. Included herein is a system wherein the deviation of an aircraft relative to its landing path is detected by a remote radio signal.

SEE OR SEARCH THIS CLASS, SUBCLASS:

189, for a system wherein the deviation of an aircraft relative to its flight path is detected by a remote radio signal and see (1) Note above.