Hybrid centered head-down aircraft attitude display and...

Communications: electrical – Aircraft alarm or indicating systems – Nonalarm flight indicator

Reexamination Certificate

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C073S17800T, C701S004000

Reexamination Certificate

active

11249237

ABSTRACT:
Methods and apparatus are provided for displaying terrain and attitude data symbology for an aircraft. The apparatus is a hybrid centered head-down display for an aircraft having a monitor configured to generate a display and a processor coupled to the display. The display has a centerline. The processor is configured to calculate a displayed drift angle limit, a displayed drift angle, align the centerline of the display with reference to the displayed drift angle, and generate on the display a first symbol corresponding to a terrain and a second symbol corresponding to an attitude of the aircraft. The processor is further configured to center the first symbol and the second symbol with reference to the centerline.

REFERENCES:
patent: 4786905 (1988-11-01), Muller
patent: 5745054 (1998-04-01), Wilkens
patent: 6853315 (2005-02-01), Schiller et al.
patent: 2003/0132860 (2003-07-01), Feyereisen et al.
patent: 2004/0160341 (2004-08-01), Feyereisen et al.
patent: 2006/0164262 (2006-07-01), Wyatt et al.
patent: 1209922 (1970-10-01), None
EP Search Report, 06121880.6, Feb. 20, 2007.

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