AVIONIC DISPLAY SYSTEMS AND METHODS FOR GENERATING VERTICAL SITUATION DISPLAYS INCLUDING INSTABILITY PREDICTION AND AVOIDANCE SYMBOLOGY

Avionic display systems (10) and methods (40) are provided for generating avionic displays (28) including instability prediction and avoidance symbology (32, 68, 70, 72, 84, 86), such as dynamically-adjusted drag device deployment cues (32). In one embodiment, the avionic display system includes a c...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: DE VILLELE, Dorothee, YASHODHAR, Veeralla Sai V, PULIKOT, Ranju Thomas, CHAUBEY, Rajesh, GUPTA, Abhishek, ADVANI, Sharanabasappa
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:Avionic display systems (10) and methods (40) are provided for generating avionic displays (28) including instability prediction and avoidance symbology (32, 68, 70, 72, 84, 86), such as dynamically-adjusted drag device deployment cues (32). In one embodiment, the avionic display system includes a controller (12) and an avionic display device (14) on which an avionic display, such as a Vertical Situation Display (VSD), is generated. The controller is configured to: (i) project (46) whether an unstable aircraft state will occur during an approach flown by an aircraft; (ii) when an unstable aircraft state is projected to occur, determine (48, 50) whether implementation of an optimized drag device deployment scheme can prevent the projected unstable aircraft state; and (iii) if implementation of the optimized drag device deployment scheme can prevent the projected unstable aircraft state, generating (52) symbology on the avionic display indicative of the optimized drag device deployment scheme.