VORRICHTUNG ZUR UNTERSTÜTZUNG DER FLUGZEUGLENKUNG IN DER LANDEANFLUGSPHASE ZUM LANDEN

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
LanguageGerman
Published 15.05.2009
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Summary: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 out transition between the two guiding modes corresponding to initial and terminal phases, respectively. A display system (9) displays activation of the control system on navigation and primary flight displays (12, 13).
Bibliography:Application Number: AT20070730970T