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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Bibliographic Details
Main Authors HUYNH, JEAN-PHILIPPE, ROUQUETTE, PATRICE
Format Patent
LanguageEnglish
French
German
Published 05.11.2008
Subjects
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