Converter for converting a load factor command into a...

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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Details

C701S004000, C701S008000, C244S07600R

Reexamination Certificate

active

08046118

ABSTRACT:
The invention relates to flight control systems for aircraft, which have large control loops delivering load factor commands and which are applied to flight controls more suited to the following by the pilot of a longitudinal attitude deviation instruction than to the following of a load factor instructions. It consists of a small control loop generating a deviation indicator displayed by the flight director on the PFD screen, with a converter for converting a controlled load factor into a longitudinal attitude deviation instruction comprising a bandpass filter allowing the integration for the calculation of the longitudinal attitude deviation instruction value in the piloting frequency span only.

REFERENCES:
patent: 5213282 (1993-05-01), Gold et al.
patent: 5823479 (1998-10-01), Nield et al.
patent: 6273370 (2001-08-01), Colgren
patent: 2004/0010354 (2004-01-01), Nicholas et al.
patent: 0485263 (1992-05-01), None
patent: 2747204 (1997-10-01), None
patent: 2841008 (2003-12-01), None
patent: 2874204 (2006-02-01), None

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