DEVICE FOR AIDING THE PILOTING OF AN AIRCRAFT DURING AN APPROACH PHASE FOR THE PURPOSE OF LANDING
The device has a control system (10) e.g. flight control unit, including control units (11A-11n) for controlling a pilot of an aircraft in two guiding modes. A calculation system (7) determines vertical and lateral deviations related to the guiding modes. A guidance system (8) automatically carries...
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
05.11.2008
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Subjects | |
Online Access | Get full text |
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