SYSTEM ZUR STEUERUNG EINES FLUGZEUGES, ZUMINDEST ZUR STEUERUNG DES FLUGZEUGES BEI UNGENAUEM LANDEANFLUG UND DER DARAUF FOLGENDEN LANDUNG

The system has information processing unit (3) processing information from sources. The unit has a multi-mode receiver aiding in landing and implementing a precision approach. An assisted approach mode function is integrated in the receiver and implements a non-precision approach by determining late...

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Bibliographische Detailangaben
Hauptverfasser: TATHAM, GILLES, PEYRUCAIN, ERIC
Format: Patent
Sprache:ger
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Zusammenfassung:The system has information processing unit (3) processing information from sources. The unit has a multi-mode receiver aiding in landing and implementing a precision approach. An assisted approach mode function is integrated in the receiver and implements a non-precision approach by determining lateral and vertical deviations between an effective position and a position that it would have if it was on a virtual approach axis. An independent claim is also included for an aircraft having a piloting system.